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Modelling the Behaviour of Microbubble Contrast
Agents for Diagnostic Ultrasound
Chien Ting Chin
A thesis submitted in conformity with the requirements for the degree of Doctor of Philosophy
Graduate Department of Medicd Biophysics University of Toronto
@ Copyright Chien Ting Chin 2001
Nationai Liimy I f F l ,canada Bibliothèque nationale du Canada
Acquisitions and Acquisitions et Bibiiographic SeMces servicm bibliographiques
The author has granted a non- exclusive licence dowing the National Lïb~ary of Canada to reproduce, loan, distn'bute or sell copies of this thesis in microform, paper or electronic formats.
The author retahs omership of the copyright in this thesis. Neither the thesis nor substantial extracts fiom it may be p d e d or otherwise reproduced without the author's permission.
L'auteur a accordé une licence non exchisive permettant a la Bibliothèqye nationale du Canada de reproduire, prêter, distn'buer ou vendre des copies de cette thèse sous la fome de micmfiche/fihn, de reproduction sur papier ou sur format électronique.
L'auteur conserve la propriété du droit d'auteur qui protège cette thèse. Ni la thèse ni des extraits substantiels de ceHe4 ne doivent être imprimés ou autrement reproduits sans son autorisation.
Modelling the Behaviour of Microbubble Cont rast
Agents for Diagnostic Ult rasound
Chien Ting Chin
Doctor of Philosophy, 2001
Department of Medical Biophysics
University of Toronto
Abstract
Encapsulated microbubble contrast agents that can be injected intravenously constitute one
of the most important developments in recent years in ultrasound imaging. These microbub-
bles oscillate nonlinearly in dtrasound fields and produce nonlinear echoes which can be
detected by novel imaging methods. The performance of these novel methods depends
strongly on the characteristics of nonlinear scattering by the bubbles. Currently a sys
tematic approach to optimizing them does not exist. This is due in part to the lack of a
theoretical rnodel for predicting the acoustic response of microbubble contrast agents. This
thesis presents some developments made to address this deficiency.
A theory for the nonlinear motion of a single bubble formed the basis of this study.
The modei was extended to account for the multipiicity of bubble size and the heterogeneity
of the dtrasound field. Experiments were designed and performed to quantitatively test
the rnodel. The resuits generdy confirmed the validity of the model, while some quantita-
tive discrepancies led to the hypothesis that the s h d plays an important role in nonlinear
scattering, which was aIso confirmed by experiment.
Contents
Abstract
Dedicat ion
List of Figures
Chapter 1 Introduction 1
1.1 Contrast Agents in Medicd Imaging . . . . . . . . . . . . . . . . . . . . . . 1
1.2 Physics of Microbubble Contrast Agents . . . . . . . . . . . . . . . . . . . . 6
1.2.1 Acoustic Impedance and Scattering . . . . . . . . . . . . . . . . . . . 6
1.2.2 Oscillation of Bubbles . . . . . . . . . . . . . . . . . . . . . 8
1.2.3 Basic Behaviour of Rayleigh's Mode1 . . . . . . . . . . . . . . . . . . 11
. . . . . . . . . . . 1.2.4 More Sophisticated Models of Bubble Osc~ations 14
. . . . . . . . . . . . . . . . . . . . 1.3 Other Behaviour of Bubbles and Cavities 17
3 Dissolution of Microbubbles . . . . . . . . . . . . . . . . . . . . . . . 17
1.3.2 CavitationPhysics . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
1.3.3 Sonolirminescence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4 Nonlinear Imaging 25
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.1 Linearity 25
. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.2 Harmonic Imaging 27
. . . . . . . . . 1.4.3 Noniineax Propagation and Tissue Hannonic Imaging 27
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.5 Thesis Outline 31
Chapter 2 A Population Mode1 of Contrast Microbubbles 33
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1 Introduction 34
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2 Theory 37
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Single bubbIe 37
. . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.2 Secondary scattering 42
. . . . . . . . . . . . . . . . . . . 2.2.3 Echoes from suspensions of bubbles 44
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3 Resdts and Discussion 45
. . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3.1 Single bubble mode1 45
. . . . . . . . . . . . . . . . . . . . 2.3.2 Prediction of population response 31
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4 Conclusions 54
Chapter 3 Experimentd Verificat ion 57
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.1 Introduction 58
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.2 Method 60
3.3 R d ts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 66
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4 Discussion .. Ti
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.5 Conclusions 73
vi
Chapter 4 Effects of Shell Disruption 75
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.1 Introduction 76
4.2 Method . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.3 Results 82
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.4 Discussion 83
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.5 Conclusions 89
Chapter 5 Applications and Future Prospects 90
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1 Introduction 90
. . . . . . . . . . . . . . . . . . . 5.2 Recent Developments in Contrast Imaging 91
. . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.1 Intermittent haging 91
. . . . . . . . . . . . . . . . . . . . . . . . 5.2.2 Pulse Inversion Detection 92
. . . . . . . . . . . . . . . . . . . . . . . . 5.2.3 Power Modulation Imaging 96
. . . . . . . . . . . . . . . . . . . . . . . . 5.3 Applications of the Bubble Mode1 99
. . . . . . . . . . . . . . . . . . . . . 5.4 Nonlinear Scattering at High Frequency 106
Chapter 6 Conclusions 110
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1 Summary 110
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.2 Limitations 111
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.3 FutureDîrections 112
. . . . . . . . . . . . . . . . . . . . . . . . . . . 6.3.1 Single Bubble Mode1 112
. . . . . . . . . . . . . . . . . 6.3.2 Evoiution of the Bubble Sizes In Vivo 114
Bibliography
List of Figures
1.1 The appearunce of contrast agents Wat increase backscatter, attenuation, or
speed of sound in the tissue. Notice that, in the image for inmeased speed of
sound, the bottom of the region containing the contrast agent is distorted along
. . . . . . . . . . . . . . . . . . . . . . . . . . . . with the connectiue tissue. 4
1.2 An idetzlized bubble system. A sphere filled with o gas zs sumounded by a
boundless region of liquid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
1.3 Resonant hepencies of bubbles from 1 to 10 Pm, calculated from Mnnaert 's
Jomulu (1.1 3) und Shima 's formula (1.14). . . . . . . . . . . . . . . . . . . 13
1.4 The scatterkg cross-section of an isolated Rayleigh bubble oscillator to 5 MHz
ultrasound. Notice thot ut higher t r a m i t t e d amplitudes, the resonant bu6 ble
szze for a fized frequency is shified d o m signzficantly. . . . . . . . . . . . . . 14
1.5 Scattered echo spectra from a 0.95 pm radius exposed to 5 MHz ultmound.
Each spectrum is normalized to the transmitted amplitude. A s the tmnsmitted
amplitude is increased, the second and higher harmonic components are in-
creased; at the highest t ~ a m i t t e d amplitude, the echo spectrum becomes very
broad and the harmonic peaks are no longer distinct. . . . . . . . . . . . . . 15
1.6 The shrinkage of bubble as a result of gas dzssoivtion and dzffùsion. Each
curve represents the euolution of a bubble piaced in water znitially saturated
uniformly with air ut 1 atm. As the bubble shrinks, the e&cf of surface tension
increases and the shrinkage rate accelerates. The Cumes corresponds to bubbles
yith initial diameters of (from the bottom) 2, 3, 4 , .. ., 10 pm. . . . . . . . 20
1.7 Operation of hannonic imaging. . . . . . . . . . . . . . . . . . . . . . . . . 28
1.8 Nonlinear distortion of a large amplitude sound vave an water due to convec-
tion (middle panel) and nonlznear bulk modulus (right panel). The distortion
is built up ouer distance (2) trauelled. . . . . . . . . . . . . . . . . . . . . . 30
1.9 Calcdated transverse beam profiles on the focal plane showing 2 MEIt fun-
damental (solzd), 4 MHz fundamental (dots), and 4 MHz second harmonies
from the 2 MEIt beam (dushes). Al1 curves vere normalized. Reproduced from
Christopher (1997). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31
2.1 Each bubble in the sample volume contributes a different wauefonn to the final
. . . . . . . . . . . signal depending on zts siie and locot incident amplitude. 45
2.2 Measured transmitted pulse used for simulation. . . . . . . . . . . . . . . . . 47
Four types of calculated response to the two-ycle wave, in tenns of radius
change (lef) and radiuted pressure (right) at 40 mm. (a), (b) and (c) Re-
sponses of 1.2 Pm, 6.0 pm and 3.0 pm diameter bubbles to 5 kPa peak-to-peak
incident amplitude. (d) Response of the 3.0 pm bubble to 100 kPa incident
amplitude. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Calculateci findumental (top) and second hamonic (bottom) cross-sections ( in
rn2) of single bubbles to Pin (t) . The grey level represents lineorly the cross-
sectional areas. The tick m a r k dong the top and right edges of the figures
. . . . . . . . . . . . mark the exact mdài and amplitudes of each calculation.
(a) Measured sàze distribution of bub ble ensemble. (b) Meusured transducer
. . . . . . . . . . . . beam profile B(a) uped in calculation of agent response.
Nonnalàzed Fourier spectra of the simulated buk agent echoes. The spectra
were nonnalàzed by dàvàding by the square of the incident amplitude. The grey
levet represents dB sctale. Notice spectral broadenzng of the honnonic peaks at
hzgh incident amplitudes. . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fundamental (top) and second harmonic (bottom) responses of simulated agent
os a function of incident focal amplitudes at three frequencies. The error bars
indicote standard evor of 32 simulated ensembles. . . . . . . . . . . . . . . .
. . . . . . . . . Experimental setup for the nonlinear scattering meusurement.
F i u m i t t e d four-cycle (left) and one-cycle (right) w a v e f o m and the corne-
spondincl fTemenm mectrurn fbottorn) used in both simulation and emerinrent.
Site distribution of bvbbles used in calculation and the the beam profles of the
tmnsducers used in eqerirnent. . . . . . . . . . . . . . . . . . . . . . . . . . 64
Power spectra of simulated zesponses from the four-cycle (top) and one-cycle
(bottom) pulses. The numbers represen t incident peak- to-peak focal amplitude. 65
Power spedza of scattered signal from the four-cycle (top) and one-c ycle (bot-
tom) pulses. Numbers represent incident penk-to-peak amplitude. . . . . . . . 67
Stmulated and measured scattenng c o e m e n t s vs. ancident amplitude in re-
sponse to the four-cycle pulpe. (top) Fundamental ( f o ) and second hannonic
(2 fo); (bottom) spectral bruadening (1.5 fo). Error bars in the simulated resuits
indicate standard error using 32 ensembles. . . . . . . . . . . . . . . . . . . . 69
Simvlated and measured scattering cueficients vs. incident amplitude in re-
sponse to the one-cycle pulse. (top) findamental (/O) and second hannonic
(2 fo); (bottom) spectral broadening (1.5 f , ) . Error bars in the simulated results
indicate standard e m r uskng 32 ensembles. . . . . . . . . . . . . . . . . . . 70
Optison echoes from exposvre to 2.0 MHz pulses ut a puise repetition frequency
of 2 Mz and peak-to-peak amplitude of 3.6 MPo. The first, third and twentieth
echoes demowtmte bubble shell disruption. The bubbles had not been exposed
to u l tmound pnor to the first pulse. Significantly elevated fundamental and
h a m o n i c scattenng are obserued ofter initial exposuze, but by the twentieth
. . . . . . . . . . . . . . . . . . echo, the bvbbles have virtualty d i sappead 72
. . . . . . . . Experimental setup for the nonlinear scattering measu~ement.. 79
4.2 The puking sepuence used in the shell effects rneasurement. . . . . . . . . . . 81
The l s t , I l th , 21st, 31st and 41d echoes from one of the measured data set
for the regular Definity (PFC) and the special Definity (fi). Each trace was
10 p in length. P R . = 2 M z , p, = 1.8 MPa. The PFC echoes (voltage)
were scaled by a factor of 4.46 since the spen'al N2 Defin* v a s a weaker agent. 83
Lifetimes (deJined as tirne for the RMS amplitude of the echoes to drop to half
the mozi'mvrn level) us. incident amplitude for h o agents with different gas
types . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Pairs of echoes from Sonauist @nt different jîrst pulse amplitudes (p,). The
delay between the fist und second echoes is 15 p. Each trace was 5 ps in
length and was nomalired by the corresponding (fkst or second) inczdent am-
plitudes. Notice that at the hzghest p,, 60th the first und second echoes were
elevated. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . First pulse scattering coeficients for the four contrast agents
. . . . . . . . Second pdse scattering coeficients for the four contrat agents
m e n a high axial resolution is desireà, generolly a v ide bandwidth is used.
However, the abzlity of hamonàc àmaging to discriminate between fundamental
. . . . . . . . and harmonzc frequencàes is limited by overlapping bandwidths.
Pulse Inversion Detection. A pair of incident pulses with opposite szgns are
tmnsmitted. The echoes are summed together, the fundamental cornponent is
cancelled out and the men hannonie components are preserued. The echoes
were culculated for a 1.9 pm diameter fiee bubble. Incident peak-to-peak am-
plitudes were 300 kPa and 150 kPa. . . . . . . . . . . . . . . . . . . . . . . .
5.3 Power Modulation Imaging. A pair of incident pulses with different amplitudes
are tmnsmitted. A wezghted difference of the echoes is used to cancel the
lineur component. Ail harmonic cornponents are preserved. The echoes were
culculated for a 1.9 pm diameter free bubble. Incident peak-to-peak amplitude
was300kPa. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 98
5.4 Pulse Inversion Detection (PD) and Power Modulation Imaging (PMI) em-
ploy the limited bandwidth of the transducer di#erently. The dashed line repre-
sent the frequency response of a hypothetical transducer with 100% banduridth.
PID benefits M m a higher nonlznear response, while PMI benefits frorn the
full exploitation of the trunsducer bandwidth. . . . . . . . . . . . . . . . . . 100
5.5 Scattered woveforms of a 1.9 pm bubble in response to a 5 MHz incident pulse
(FWHM pulse duration = 1.2 cycles). Each wavefonn is nonnalized by the
incident pressure. Sixteen di 'eren t incident pressures (peak- to-peak) spanning
1 to 1000 W a were simulated. . . . . . . . . . . . . . . . . . . . . . . . . . 101
5.6 Result of P D (top) and PMI (bottom). The Y-& values correspond to the
amplitude of the first (stronger) pulse. Each wavefonn is nonnalized by the
incident pressure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 102
5.7 h p e n c y spectra of single puise echoes (top), and the results of the PID
(middle) and PMI (bottom) rnethods. The nurnbers next to the Cumes indicate
the peuk-to-peak incident amplitudes. . . . . . . . . . . . . . . . . . . . . . . 104
5.8 Assumed fïequency response of the hnsducers for the cornparison of PID us.
PMImethods. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105
5.9 Relatiueperfonnance of PID and PMIusing thef7equency responses infigure
5.8. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105
5.10 Szmulated bubble echo spectra for: 0.65 pm bubbles in 20 MHz ultmsovnd
pulses ut 200 kPa (black) and 4.0 prn bubbles in 2 MHz ultrasovnd pulses at
50 kPa (red). The echo power from the smaller bubbles was h r e ~ e d by a
factor of 6.3 to account for the higher number density. . . . . . . . . . . . . 107
5.11 Averuged poww spectra of 1000 echoes for Definity (solid) and graphite pow-
der (dashed). The result frorn graphite powder demonstrate second and third
hannonics (40 and 60 MHz) due to nonlinear propagation; the additional 2329-
nals at these peaks, as well as spectral broadening, are due to the nonlinear
scatterhg by the contrast bubbles. . . . . . . . . . . . . . . . . . . . . . . . . 108
Chapter 1
Introduction
1.1 Contrast Agents in Medical Imaging
Medical imaging systems produce images of the human body by probing it with radiation
such as X-rays, electromagnetic waves and sound waves. Diagnostic information can be
deduced because these radiations interact Mth the body tissue and encode information
about some physical or chernical properties of the tissue. Image contrast results hom the
consequent relative ciifference in the detected mgnd amplitudes from different regions of
target tissue. Each imaging modality relies on a different contrast mechanism. X-ray imaging
reiies on Mnations in atomic number and electron density. Magnetic resonance imaging relies
on variations in hydrogen atom density and interaction with large molecules. Ultrasound
irnaging relies on microscopie k a t i o n in density, bulk modulus and mechanicd relaxation.
WhiIe these methods have proved tremendously usefid, theh abiiity to detect and localize
some disease-related structural changes in tissue, partinilady on a fine scale, is often Limited.
This is due to the fact that these diseases do not produce conspicuous changes in the relevant
physical and chernical properties. In many applications, foreign materids can be introduced
b i d e the body to create or enhance the vaxiations in the relevant physical or chernicd
properties. These materids are called contrast agents.
For X-ray imaging, the most common contrast agents are barium and iodine. Bariurn
sulphate "milk" is ingested by the patient, and by virtue of its high electron density (54 per
ion, compared to 18 per calcium ion), opacifies the lumen of the digestive tract. Iohexol is
a compound containing iodine, and is usually used at a concentration of 180-300 mg/ml.
Dosage of 5 to 100 ml can be injected via a catheter to enhance digital subtraction angiog-
raphy or computed tomography of the cerebral arteries, the coronary arteries and peripheral
vessels. Intravenous contrast agents allow computed tomography (CT) images to display
vascular information, otherwise absent hom unenhanced images. Nonvascular applications
include imaging of the bile duct and the fallopian tubes.
The most common of the rnagnetic resonance imaging contrast agents is Gadolinium-
DTPA (Gd-DTPA). The uncharged Gd atom is paramagnetic and creates a local inhomo-
geneity in the static rnagnetic field (Bo). This local inhomogeneity enhances the relaxation of
rnagnetic moments in the hydrogen nuclei. Both Tl and T2 relaxation times are shortened
by the presence of the Gd atoms, but the Tl shortenhg is more pronounced and can be
more reliably measured. Thus the signal from tissues perfbsed with the Gd-DTPA molecules
are enhanced in Tl-weighted Maging. Gd-DTPA is a s m d molecule and can diffuse freely
out of blood vessels and enter the interstitinm quickly. The useful irnaging tirne window
for vascular imaging is limited to about 1-5 minutes, and in most cases no more than 20
minutes. It is interesting to note that timing is so cntical in MRI that a study was initi-
ated to investigate the feasibility of using an ultrasound contrast agent to determine optimal
bolus timing for contrast enhanced MR angiography (Prince et al. 1999). More recently,
blood pool contrast agents consisting ofvery large molecules (up to 94 000 Da) with multiple
Gd ions have become avaliable (&OR and de Roos 1999). By limiting the diffusion of the
agent through the endothelid membrane, these agents can recirculate in the vascular system
dlowing imaging for a longer period of time. UseM enhancement couid be seen for up to
120 minutes after contrast injection.
Nuclear imaging depends on radiophmaceuticals as a source of ionizing radiation.
Radiophannaceuticals have the advantage that many elements exist in radioactive isotope
foms which are either found naturally or can be made by methods such as neutron bom-
bardment. Detecton of ionizing radiation are tremendously sensitive, only a small number of
radioactive atoms is needed in order to produce a useful image. It is possible to manufacture
radiophaxmaceuticals which are chemically identical to physiological molecules. These ra-
diopharmaceuticals accumulate in the tissue where the desired physiological function occurs
and produce a spatial map of some metabolic hinction in the body. For euample, Thalium-
201 is a potassium analogue which is taken up by myocytes that axe actively contractîng.
Therefore, nuclear imaging qualifies uniquely to be c d e d functional imaging.
Ultrasound contrast agents have become clinicdy relevant in the last few y e m . The
mechanisms of ultrasound contrast agents may involve modifying the backscatter, attenua-
tion or speed of sound in the tissue (Ophir and Parker 1989). Figure 1.1 illustrates concep
tuaily the images that remit kom these three types of agents. Of these, the modification of
CHAPTER 1. INTRODUCTION
n U itrasound Probe
Tissue Bearhg Contrast Agent - . c Connective
Tissue
Figure 1.1: The appeumnce of contra& agents that inmase bockscatter, attenuatzon, or speed
of sound in the tissue. Notice that, in the image for rnc-ed speed of sound, the bottom of
the region wntainzng the contrBst agent is distorted along uith the connective tissue.
backscatter is the most important, since, in this case, changes in the image coincides with
the location of the agent. Agents with difFerent attenuation or speed of sound modify the
appearance of tissues behind the agent-bearing region. This thesis will focus on agents that
modify the backscatter, in particular, agents that produce nonlinear backscatter.
Most ultrasound contrast agents are based on gas bubbles, which are very effective
scatterers of ultrasound. Gramiak and Shah (1968) were the fkt to exploit contrast created
by bubbles. They created free air bubbles by injecting saline via a catheter into the aortic
arch. However, catheterization is an invasive procedure and direct injection of gas bubbles
risks emboiism of sensitive organs such a s the brain, kidneys and lungs. A clinicaily useful
agent should be intravenously injectable and must be small enough to pass through the
capillaxies of the lungs and spianchnic beds. However, micron-size free bubbles are inherently
unstable and tend to dissolve within seconds. Therefore, imaging of gas bubbles has not been
feasible except by the direct injection into the imaged regions using a catheter. In recent
years, technologies have been developed to stabilize the microbubbles. There are two main
approaches, the k t is the encapsdation of the bubbles by a shel1 which limits the transport
of gas across the gas-liquid interface. The second is the substitution of the air wi t h a high
mo1ecda.r weight gas which has a low solubility and difisiviv. Such technologies dlow
microbubbles to survive in the body for severd minutes or longer. The first encapsulated
agents, such as EchovistTM (Schering AG, Berlui), were too large to pass through the capilary
bed in the lungs. These agents must be injected intra-arteridy in order for the left heart to
be imaged. Newer agents, which began with the air-aibumin Albunex (MLlallinckrodt Medicd
Inc., St. Louis, MI) (Feinstein et id. 1990), are d c i e n t l y small and stable to appear in
CHAPTER 1. INTRODUCTION 6
the systemic circulation following intravenous injection. These new agents are suspensions
of microbubbIes containhg a range of diameters from below 1 pm to about 5 Pm. Invariably
a srnd number of bubbles of 10 pm or even larger are also present, however, both the
volume fraction and number fraction of these large bubbles are typically less than 1%. The
bubbles rnay contain air, a perfluorocarbon (PFC) gas or a mix of the two. The bubbles of
most agents are encapsulated by a sheil composed of surfactant, polper , or lipid. There are
currently over twenty agents in various stage of development and trials, several of which have
received approval for clinical use in Europe, the US and Canada. Next, we shall consider
the phyiscs of ultrasound contrast agents.
1.2 Physics of Microbubble Contrast Agents
1.2.1 Acoustic Impedance and Scattering
Diagnostic ultrasound is non-invasive, inexpensive and widely available and employs no ion-
izing radiation. The basic approach is based on radar-like pulse-echo rnethods. A transducer
is used to convert electrical pulses to ultrasound and vice versa. Pulses of ultrasound are
directed into the body and allowed to interact with the body structures. A fraction of the
dtrasound energy is scattered back towards the transducer which converts it back into an
electrical signal. These backscatter signais (echoes) contain information about the acous-
tic properties (scattering, attenuation and speed of sound) of the body structures. The
most commonly desired properties of an dtrasound contrast agent are high backscatter, lom
attenuation and identical speed of sound to biological tissues.
CHAPTER 1. INTRODUCTZON 7
Scattering occurs when sound is transmitted through a region with varying acoustic
impedance. Acoustic impedance of a materid is given by
where p is the density and c is the speed of sound. In iiquids and solids, speed of sound is
given by
where ,LI = pdpldp is the bulk modulus of the medium. The speed of sound of a gas is given
by -
where p is the pressure and 7 = %/c, is the ratio of the coefficients of specific heat at
constant pressure and constant volume, respectively. At the boundary between the different
media, dtrasound is partially reflected. Refiected energy is related to impedance by
where Zi and Z2 are the acoustic impedances of two different media. Water has an impedance
of 1.5 x 106 Pa-m/s. Contrast materials should be made of material with a significantly
higher or lower impedance. Good candidates are gases (2 = 330 Pa-m/s) and inorganic
solids (such as steel with Z = 23 x 106 Pa-m/s). Of the two, a gas is both a stronger
scatterer and a more easily metabolized materid. Ekperimental work has &O shown that
contrast agents consisting of gas-filled microbubbles are more effective (Ophir and Parker
1989). Therefore, aùnost all the ultrasound contrast agents in use or in developmeni are
based on gas microbubbles.
1.2.2 Oscillation of Bubbles
Due to the large dserence in bulk moduli between water and gas, bubbles are in fact
oscillators. The heavy and nearly incompressible liquid functions as the m a s , and the light
and highly compressible gas functions as the spnng in the classic mass-and-spring mode1 of
oscillators. Consider the simple system in figure 1.2 in which a sphere Nled with a gas is
surrounded by a boundless region of liquid. Assuming the liquid to be incompressible and
Figure 1.2: An idealized bubble system. A sphere jilled vith a gas as surrounded by a boundless
irrotational, the velocity at any point in the Liquid is purely radial and is related to the
CHAPm' 1. n\rTRODUC!TTON
instantanmus velocity of the bubble radius R:
Throughout this thesis, a dot above a variable indicates totd t h e derivative, 2 = dx/dt .
Assuming the mas of the gas to be insipificant compared to the iiquid, the kinetic energy
of the liquid can be calcdated as
K.E. = lm u24rr2dr = 2p7rff' R2, 2 R
where u is the velocity of the liquid at a distance r from the centre of the bubble. The
potential energy of the gas is aven by
where pg is the pressure inside the bubble and Ro the equilibrium bubble radius. .Assuming
the expansion and compression of the gas to be adiabatic, pg is given by
where pso, &, it$ and 7 are the eqniübrium intemal pressure, bubble radius, bubble volume
and ratio of specific heat capacities respectively.
The equation of motion of the bubble boundary c m be obtained by stipulating the
C W T E R 1. INTRODUCTION
time-derivative of the total energy (K.E. + P.E.) to be zero, the result is
Equation (1.9) was derived by Rayleigh (1917), supposedly, to study the creaking noise
produced by a kettle of water just before boihg (Flynn (1964) noted that Lord Rayleigh
was dso commissioned by the Royal Navy to study propellor damage caused by bubbles).
While Rayleigh originally on?y considered a cavity collapsing without e-xtemal forces, it is
easy to allow for the bubble to be driven by an applied pressure wave p,, giving
By numerically integrating equations (1.10) one can calculate R(t) in response to an incident
pressure wave pin. Since particle velocity at any point in the liquid is given by equation
(1.5), the radiated pressure c m also be determined. Rom the radiated pressure, a scattering
cross-section, defmed as total radiated power divided by incident intensity, can be calculated.
While many of the assumptions used make equation (1.10) invaiid for quantitative prediction,
Rayleigh's mode1 nonetheless dernonstrates many behaviours that are characteristic of the
acoustic response of contrast bubbles.
1.2.3 Basic Behaviour of Rayleigh's Model
By drawing analogy to the kinetic energy of a mass moving at a Gxed velocity, K.E. = mv2/2,
an effective mass can be defined fiom equations (1.6),
Similarly, by a binomial expansion of pg, an effective spring constant can be defined from
(1 -7):
IF,,, = 6flVgoR, (1.12)
using the potential energy stored in a spring: P.E. = k(hx)* . From the m a s and spnng
constant the resonant frequencies is given by:
Therefore, the natwal resonant hequency of a bubble oscillator is simply inversely propor-
tional to its size. Entering the appropriate values for an air bubble in water, one obtains
the resonant frequency of a 2 pm diameter bubble of 3 MHz. Fortuitously for ultrasound
imaging, the resonant fiequencies of bubbles s m d enough to pass through the capillary bed
(< 5 pm) f d within the fkequency range of diagnostic dtrasound (> 1.5 MHz), making
microbubbles particdarly efticient as scatterers of dtrasound.
Equation (1.13) was fmt derived by Minnaert (1933) and does not account for sudace
tension and damping effects. More sophisticated formulas for the resonant fkequency of s m d
C W m R 1. INTRODUCTION 12
bubbles exist and were reviewed by Shima (1970). Equation (17) and (18) of Shima (1970)'
which account for compresçibility, surface tension and viscosity for linear oscillation, are
reproduced here:
B is a constant involved in the Tait equation of state for water, and has the ernpirical value
01 3000 atm. Figure 1.3 presents the resonant frequecy calculated from Minnaertk (1.13)
and Shima's (1.14) equations. One notices t hat Minnaert 's formula begins to underesti-
mate resonant kequency by a signincant factor for bubbles smaller than 3 Pm. Minnaert's
fonnula (equation 1.13), because of its simplicity and accuracy for larger bubbles, is very
commonly quoted. It is important to remember its use should not be extended beyond
order-of-magnitude estimations for megahertz applications.
To illustrate some linear and nonluiear behaviour of Rayleigh's equation, the response
of individual bubbles to 5 M H z ultrasound is next considered. Equation 1.10 was integrated
using the third order Ronge-Kutta method. The response, as measured by the acoustic
energy scattered by the bubble, is plotted against bubble radius in figure 1.4. The power of
the bubble o s d a t o r is underscored by noting that a resonant bubble has a scattering cross-
section of approximately 25 pz, whereas a single isolated red blood cell has a scattering
0.2 I I 4 t L
0.2 0.5 1 2 5 10 20 Bubbb Diameter (pn)
Figure 1.3: Resonant /requencies of bubbles from I to 10 Pm, colcukated /rom Minnaert 's
formula (1.13) and Shima's formula (1.14).
cross-section of only 6 x 10-6 pn2, (see page 132 of Mo and Cobbold (1992)) which is about
four million times weaker. At a low transmit amplitude (1 kPa peak-to-peak), the response
is strongest from a bubble of 0.95 pm radius, in agreement with the prediction by Shima.
Hapever, at a higher transmit amplitude, the nonlinearity of the bubble motion cornes into
play and the scattering peak becomes more complicated. Most notably, the resonant bubble
size is shifted down to about 0.55 Pm.
The most important feature of the nonlinear scattered signal is the harmonic content.
Figure 1.5 shows the spectra of a 0.95 pu radius bubble in response tu 5 MHz uitrasound. At
the lowest transmitted ampütude (1 kPa) , the bubble motion was nearly perfectly linear and
ody a very minimal amount of harmonic scattering is produced. At a higher transmitted
amplitude (50 kPa), the motion is weakty nodinea. and 2nd and higher harmonic compo-
O 0.5 1 1.5 2 2-5 3 3.5 4 Bubble radius (pm)
Figure 1.4: The scattering cross-section of an àsolated Rayleigh bubble oscillator to 5 MHz
ultmsound Notice that at hzgher transmitted amplitudes, the resonant bub ble szze for a fixed
frequency is shified down szgnaficBntly.
nents are evident. At the highest transmitted amplitude (1 MPa), the motion is strongly
nonlinear and scattered waves have very broad bandwidth. Harmonic peaks, in fact even
the huidamental peak, are no longer clearly distinct from each other.
1.2.4 More Sophisticated Models of Bubble OsciIIations
Since Rayleigh studied the idealized case of a spherical void freely collapsing in a liquid in
1917, rnany authors have contributed various extensions to Rayleigh's equation to account
for various red world effects. These include the gas (typicdy air) pressure, the vapour
pressure (of the liquid), surface tension, viscosity, compressibüity of the üquid, mas transfer
(dissolution and effervescence of the gas), thermal t r d e r and gravity. Mathematicdy, a
Figure 1.5: Scattered echo spectra from a 0.95 pm radius ezposed to 5 MHz ultrasound.
Each spectrum is nomalized to the tmmitted amplitude. A s the tmnsmitted amplitude is
znmased, the second and hzgher hamonic components ore increased; at the hzghest t m m i t -
ted amplitude, the echo spectnnn becomes uery broad and the hamonic peaks are no longer
distinct.
mode1 of spherical bubble oscillations can be understood as a basic differential equation that
describes the flow of the liquid outside of the bubble, and a set of boundôry conditions and
correction terms. Considered this way, the most important component is the compressibility
of the liquid. The basic differential equation is essentially an equation for the dynamics of
the liquid. When the liquid is incompressible, the differential equation is given by equation
(1.10). When a linear compressibility is assumeci, Several authors (Herring 1941; Keller and
Miksis 1980; Trilling 1952) derived a more cornplex equation accounting for a compressible
liquid which supports ünear acoustic mves to propagate at a constant finite speed. Cur-
CHAPTER 1. INTRODUCTION 16
rently, the most sophisticated form of the basic equation was derived by Gilmore (Akuüchev
et al. 1968; Hidrling and Plesset 1964; Gilmore 1952), who took into account nonhear prop
agation caused by the convective component of the Navier-Stokes equation and the nonlinear
compressibili@ of wat er.
Vokurka (1986) made a cornparison of Rayleigh's, Hemng's and Gilmore's equa-
tion by numerical computation. -4s expected, when the oscillation amplitude increases,
Rayleigh's and Herring's models become l e s accurate. Vokurka measured the amplitude by
A = and he found that, compared to Gilmore's equation, Rayleigh's equation was
satisfactory for A < 2 and Herring's equation was satisfactory for A < 4.5. However, the
choice of the basic equation does not always follow simply from the oscillation amplitude.
In the theoretical study of sonoluminescence, Keller's or Trilling's formulations (which are
equilivdent to Hemng's) are often prefened despite its inaccuracy (Gaitan et al. 1992; Ka-
math et al. 1993). This is because the processes in the gas phase are far more important
in sonoluminescence than the precise dynamics in the iiquid (see section 1.3.3). Therefore,
Keller's, or even Rayleigh's, equation is used for its simplicity and clarity.
To see why the Gilmore mode1 is often avoided when possible, it is useful to consider
its mathematical form. Gilmore's equation relates the local speed of sound C and enthalpy
H (in the liquid) at the bubble w d :
where C and H are determhed by the instantaneous pressure at the bubble wall (the Tait
C W T E R 1. INTRODUCTION
equation) ,
cm, p, and p, are the (constant) speed of sound, pressure and density of the undisturbed
Iiquid. B and n are constants in the Tait equation which have the ernpirical values of 3000
atm and 7, respectively, for water. Finally, P is the pressure at the bubble wall. In cases
when P is simply equal to p, given by equation (1.8), equation (1.15) can be easily solved
numerically. However, when more mechanisms are included in P, the solving of equation
(1.15) becomes much more complicated. In some cases, such as in sonoluminescence, P itself
is determined by a differential equation that describes the mechanisms inside the gas bubble.
The internai differential equation is then coupled to the extemal differentiai equation through
the variables R and P, making the problem very costly to solve computationally.
1.3 Other Behaviour of Bubbles and Cavities
1.3.1 Dissolution of Microbubbles
Henry's law dictates that, at a fixed temperature and pressure, a gas in contact mith a
liquid will be dissolved in the liquid untii a eqilibrium concentration is reached. If the
concentration of the dissolved gas is below the equilibrium concentration, more gas wiil
be dissoIved, conversely, if the disolved gas concentration is too high (a condition called
CKAPTER 1. INTRODUCTION 18
oversaturation), the gas will evaporate out of solution to form bubbles. A common example
is beer or softdrinks which are bottled with carbon dioxide under pressure. Inside the
presninzed container, the equilibrium is rnaintained and the amount of gas dissoIved is
determined by the temperature and pressure. When the condition is disturbed, e.g., by a
rise of the temperature or more commonly by a drop in the pressure when the bottle is
opened, the equilibrium concentration is decreased, and bubbles form and grow on the side
of the glas. Another example of oversaturation is found in deep sea diving. Every 10 meters
of depth adds about one atmosphere of pressure to the diver's body. At depths of 50 m or
more, significant amount of nitrogen and oxygen can be dissolved over time into the blood
plasma. Therefore, if a diver who has been exposed to a high pressure for a penod of time
ascends too quickly to the d a c e , an oversaturation of gas develops and bubbles are formed
in the blood stream and the synovial fluid. The most obvious symptom is joint pain, which
causes the sufferers to walk slightly stooped or bent over (NOAA 1990). For this reason,
such a condition is commonly known as the "bends"; it is also called the decompression
sickness. If a large number of macroscopic bubbles are forrned, a mgnicm number of blood
vessels can be emboiized, causing damage to the brain, kidneys and lungs - even death can
be a consequence.
Typicdy, water or aqueous liquid exposed to the atmosphere (blood is partially ex-
posed to the atmosphere in the Iungs) are saturated wïth dissolved air. The concentrations
of dissdved gases are determined by the room temperature and pressure. A bubble placed
in such a liquid is inherently unstable. Surface tension exerts an additional pressure in the
CHAPTER 1. INTRODUCTION
gas phase. The additional pressure is given by
where (T is the surface tension and R is the radius of the bubble. Therefore, the gas in a 1
pm air bubble in water expenences a 72.5 kPa overpresmire, which amounts to about 70%
of the ambient pressure. The pressure difference between the gas phase and the liquid phase
causes an inequilibrium and the gas will be gradudy dissolved. As the gas is dissolved, the
radius of the bubble shrinks, causing the pressure difference to continue to increase according
to equation (1.17). Therefore, an air bubble in a liquid saturated with air (relative to the
room pressure) will g a d u d y dissolve at an accelerating pace.
As the gas dissolves, a concentration gradient n e u the bubble boundary is established.
The rate of dissolution is ümited by the localIy accumulated concentration in the surrounding
liquid. In the absence of flow, difision is the mechanism by which the dissoived gas molecules
are transported outward kom the bubble boundary. Epstein and Plesset (1950) and Neppiras
(1980) derived an equation br the evolution of the radius of a bubble placed in a liquid
ini t idy containing a uniform concentration of dissolved gas:
where D is the diffusivity constant Cs is the equilibrium concentration, Cm is the initial con-
centration, p, is the densi@ of the gas ( approda ted to be constant) and p , is the ambient
pressure. Equation (1.18) cm also be used to predict bubble growth under oversaturation.
Solving equation (1.18) for free air bubbles under an ambient pressure of 1.0 atm yields
lifetimes of 10 ms to 6 s for bubbles of 1 to 10 pm diameters (see figure 1.6).
"O 0.2 0.4 0.6 0.8 1 1.2 Time Isec'l
Figure 1.6: The shrinkuge of bubble as a result of gus dissolution and diffusion. Each curue
represents the euolution of a bubble placed in water ànitially saturated uniformly with air at
1 atm. As the bubble shrinks, the effect of surface tension increuses and the shrinkage mte
accelemtes. The curves corresponds to 6ubbIes with initial diameters of (/mm the bottom) 2,
3, 4, ..., 10 Pm.
Experirnentally measured lifetirnes tend to be &able and somewhat longer than
that shown in figure 1.6. It is believed that irnpurity in the experimental system acts as
a surfactant which coats the bubble and reduces the gas dissolution (Neppiras 1980). On
the other hand, liquid 0ow relative to the bubble (caused by, for example, Boatation of the
bubble) c m sipniIicant1y accelerate the dissolution process. This is due to the fact that
dissoIution is ümited by the concentration gradient 6eId in the iiquid and any convection is
bound to help to equilibrate the concentration gradient.
1.3.2 Cavitation Physics
Cavitation is a Ioose t e m used to describe the formation, dynamics and effects of a cavity or
small bubble caused by mechanicd stress or sound waves (Knapp et al. 1970). When a solid
object is moving in a Liquid, the pressure drops according to the Bernoulli equation (or more
precisely the Navier-Stokes equation). At a moderate speed, this pressure &op can exeed
the ambient pressure. The Bernoulli equation can provide an order of magnitude estimate
of the speed needed to create a negative pressure:
For water at atmospheric pressure (about 101 kPa), this is merely 14.2 m/sec. A negative
pressure can be substained in a Liquid or solid until it reaches the tensile strength of the
material. The tensile strength of pure water is over 250 atrnospheres, but the presence of a
tiny amount of impunty, especidy dissolved gas, reduces the tende strength dramaticdy.
As a result, mechanical stress caused by common processes such as a turning propeller is
sufncient to rip apart the water and create cavities (Plesset 1949). The collapse of these
cavities can be quite violent and can cause severe pitting of matend even as hard as steel.
ExpIosives are used to create an underwater cavity tens of rneters large which then coiiapse
catastrophically (Cole 1948). In fact, depth charges damage submarines not by the shock
fiom the explosion but by the great destructive force unleashed during the collapse of the
caviw.
Ultrasound, iike mechanical stress, can also create cavitation. Acoustic cavitation has
been observed since the 1930s (Marinesco and Tri1Iat 1933) and a wide variety of phenornena
have been attributed to it (Neppiras 1980). A Ml dLscussion of acoustic cavitation is beyond
the scope of this introduction, but several effects axe of interest here. Stable cavitation is
the stable oscillation of one bubble or more commonly a cloud of bubbles in a sound field.
In contrast, transient cavitation is often obsevered in which the bubble or bubbles collapse
violently, causing erosion, emission of light, chernical and biological effects. Theoretical inves-
tigations of transient and stable cavitation formed the basis of much of what is known today
about the dynamics of bubble interaction with ultrasound. These include the development
of al1 the theories described in sections 1.2.2 and 1.2.4.
Transient cavitation is dso of interest because of the bioeffects that can be a result.
Rupture of cells in vitro and degradation of DNA molecules have been known since the
1950s (Flynn 1964). The pressure necessary to create cavitation, the cavitation threshold,
is known to be significantly higher in vivo than in untreated tap water (the t ~ e reason of
this is not yet clear, but it is generdy beiieved that the higher viscoscity of bodily Buid and
the lower concentration of dissolved gas combine to reduce the occurrence of cavitation).
Nonetheless, macroscopic lesions can be created with intense ultrasound and the safety of
diagnostic ultrasound, especially in the area of obstetrics, is of concem. To that end, FDA
enforces a maximum allowable output level on ail diagnostic scanners. The output level is
meanued with the Mechanical Index ( M I ) which is based on the potential for cavitation
CHAPTER 1. INTRODUCTION
inception. MI is d e h e d by
where p- is the spatial-peak-temporal-peak negative pressure measured in MPa and f is
the transmitted frequency measured in MHz ( Iv lZ is quoted without units). The maximum
allowable output for most applications is set at M I = 1.9. It is important to note that the
peak negative pressure p- is "derated", meanhg that the values measured in a water tank
were adjusted for expected attenuation by human tissue h m the transducer face to the focus
before being used in the cdculation of MI. Notice that at higher freqencies, the potential for
cavitation is lower and hence a higher pressure amplitude is allowed. The M I has become a
common measure of output pressure for cornparison between different frequencies. different
scanning modes and different manufacturers.
Since the onset of cavitation is very sensitive to the presence of microcavities knom a s
'huclei" , microbubble contrast agents were expected to enhance cavitation activties. Indeed,
Miller and Thomas (1996) and Dalecki et al. (1997) found that Mbunex in combination with
exposure to ultrasound can cause hemolysis (lysing of red blood cells) both in vitro and in
vivo. Skyba et al. (1998) showed contrast microbubbles can induce microvessel ruptures when
exposed to diagnostic uitrasound. These results naturally raise the question of bioeffects of
exposing tissue carrying contrast agent to strong dtrasound. However, it should be noted
that these experiments were performed in small animais in exposure conditions that are not
typicdy the case in humans. The in vivo pressure these animals were exposed to were
B&cantly higher than that allowed by the MI-regdations. At present, it is diEcdt to
extrapolate these animal results to clinical conditions in humans. However, signiticant side-
effects can be d e d out due to the large body of evidence that even mild side-effects are
rare (Nanda and Carstensen 1997). At the same t h e , Skyba et al. (1998) suggested that
these bioeffects have potential therapeutic applications. More reseaxch is needed to detect
these bioeffects in human and to determine the feasibility of e-xploiting them in therapeutic
interventions.
1.3.3 Sonoluminescence
One of the most spectacular effect of cavitation is sonoluminescence, the emission of light
from ultrasonically driven gas bubbles. Origindly observed in 1933 by Maxinesco and Trillat,
sonoluminescence presented a challenging puzzle to reserachers searching for a mechanism.
A wide vaxiety of models were proposed, including triboluminescence (light emission by
fiction), microdischarge and mechanochemical effects (Gaitan et al. l992). Systematic ex-
periments in a controlled environment were not available until the discovery in 1989 that a
single bubble (instead of a cloud) c m be driven to emit light bright enough to be seen by
the human eyes. Subsequently, rnany rernarkable characteristics of single bubble sonolumi-
nescence (SBSL) were observed. Typically a bubble of about 5 pm or larger is driven by
a 20 kHz sound field, and a flash of Lght is emitted in each acoustic cycle, that is, a flash
is emitted every 50 p. Surprisingly, the duration of the flash is extremely short compared
to the acoustic cycle, in fact, until recently the exact duration of SBSL emissions was not
h o m because none of the d i n g optical detectors had dficiently fast response. More
recently, the duration was determined to be about 50 picoseconds. Each emitted Lght flash
CXAPTER 1. INTRODUCTION 25
has a spectnim simiIar to that emitted by a body of very hot gas. Very recently, it was
declared (Apfel 1999) that a complete explanation of SBSL was obtained (Hilgenfeldt et al.
1999). In this model, violent collapses during the compression phase of each acoustic cycle
cause the gas to be repeatedy heated up to 20,000-30,000 K and compressed to 5,000-
7,000 atmopheres. During these repeated compressions, an interesting phenornenon occurs
which has the diatomic molecules (N2 and Oz) diffusing out into the liquid, leaving only
monoatomic noble gas (typicdy argon) in the gas bubble (Matula and Crum 1998). This
body of compressed, hot, noble gas is responsible for the emission of the light observed.
It is noted that the explanation by Hilgenfeldt et al. (1999) was based on a Rayleigh-
Plesset equation similar to equation 1.10 or to the equation by Trilling, which is the basis
of this thesis. The process is said to be dominated by the generation of shockwaves in the
gas phase and the gas diffusion process so that the nonlinear cornpressibilty introduced by
Giimore is not important in this consideration.
1.4 Nonlinear Imaging
1.4.1 Linearity
Linearity is understood in the context of a system which produces an output in response to
an input. Mathematicaily, we write
H is called the transfer function of the system. A system is defhed as l inex if it follows
this intuitive principle: the output from the sum of two inputs is the same as the surn of the
outputs from the individual inputs. This is represented mathematically by
where a and b are constants. In the context of ultrasound imaging, the concept of transfer
hnction is used to analyze many processes, such as transduction (conversion between electri-
c d and acoustic signais), acoustic propagation, acoustic attenuation and image processing.
Not a l l of these processes are linear, in pazticular, scattering of ultrasound by a bubble, as
described by equation (1.10), constitutes a nonlinear systern. In this case, the transfer h c -
tion H (which cannot be written in an explicit f om) does not obey the liiearity equation
(1 -22).
1.4.2 Harmonic Imaging
The second harmonic component of the microbubble echoes (see figure 1.5) offers a special
signature allowing them to be separated from tissue signais. The first nonlinear contrast
imaging method used clinicdy was harmonic irnaging (Burns et al. 1996). The operation
of harmonic imaging is depicted in figure 1.7. Like conventional imaging, ultrasound pulses
are transmitted into the human body. During reception, a simple high-pas filter removes
the fundamental component from the RF echoes, leaving mostly the signal scattered from
the contrast agent. This filtered signal is used to generate the harmonic image. In combi-
nation with the Doppler method, which detects changes in the echoes due to movement or
disappearance of the targets, hamonic imaging was demonstrated to be capable of detecting
blood flow at the microvascular level. Imaging of blood Bow in tissue perfused by 40 pm
vessels was demomtrated by Burns et al. (1994).
1.4.3 Nonlinear Propagation and Tissue Harmonic Imaging
Acoustic propagation in water, and by extension soft tissues, is not linear. While this fact has
been known both theoretically and experimentally for decades, its significance to ultrasonic
imaging was not realized until recently. This is due to the combination of two factors:
(1) eariier transducers and scanners did not have sufficient bandwidt h and sensitivity to
detect the nonlinear signal; and (2) most workers had not been searching for the nonlinear
signal because it was not expected that the harmonic signal cotdd have any applications.
This changed when severd groups noticed that harmonic imaging designed for contrast
applications not only produced a background image before the injection of the agent, but
CHAPTiE:R 1. INTRODUCTION
Transducer
Tissue
Contrast Agent
Image Formation --3- or
Doppler Demodulation
3 MHz ultmound 6 MHz ultrasound
Figure 1.7: Operation of harmonic imaging.
that the background image was of higher quality than conventional imaging.
The cornplete theoretical description of nonlinear propagation is very cornplex. But
some intuitive understanding can be achieved with a sixnplified approach. Two factors con-
tribute to the nonlinear propagation of sound waves in water. The fhst is the fact that sound
is a longidutinal wave of "wavefionts" of molecuiar displacement. Since the displacernent is
in the same direction as the wave propagation, a wavefiont is advmced or retarded depend-
ing on the amplitude and direction of particle (molecular) displacement. The phase velocity
CHAPTER 1. LNTRODUCTION
is the velocity at which a wavefiont is travelling:
where q is the speed of sound for infmitesimdy small amplitude sound waves and u is the
particle velocity. This is called the convective component of the noniinear distortion of the
propagated wave. ltanslated into pressure, this means the high pressure crest of the wave
will travel faster and "pile up" on top of the slowly propagating low pressure trough. The
middle panel of figure 1.8 illustrates this phenornenon. The second contribution to nonlinear
distortion is the nonlinear compressibility of water (also cailed the material nonlinearity).
The phase velocity, taking into account both convection and material nodinearity, is
where A and B are the coeEcients of the linear and quadratic tems in the Taylor expansion
of the equation of state of the medium. The ratio BIA is a material constant and is relatively
independent over the fiequency range 1-10 MHz. For water, Bl.4 = 5.2; for soft tissues, the
value is higher, ranging fiom 6.5 (liver) to 11 (fatty tissue).
A M y generalized nonlinear wave equation is as yet unsolved by analytical means.
Numerical eomputations are typicaüy Limited to certain specinc cases. For many situations,
the paracial (near the beam a*) field for the forward propagation of a focussed beam with
or without attenuation is simdated. A number of approaches, each invokving different sim-
plifications and approximations, are a d a b l e . These include the h i t e Merence method,
CHAPTER 1. INTRODUCTION
I Convection +
Figure 1.8: Nonlinear distortion of a large amplitude sound wave in water due to convection
(mzddle panel) and nonlinear bulk modvlvs (right panel). The distortion zs bu& up ouer
dis tance (2) travelled.
the pseudospectral method, and the KZK algorithm (for a more detailed discussion, see
Hamilton and Blackstock (1997) and Wojcik et al. (1998)). As an example, the nonlinear
beam was cdcdated using the NLP method, a variation of the KZK method (Christopher
1997). Figure 1.9 depicts the b e m profile of the second harmonic component from a 2 MHz
Gaussian focussed beam as weU as the bdamenta i bearns for both 2 MHz and 4 MHz.
The width of the main lobe of the harmonic beam is narrower than the 2 MHz fundamentd
beam but wider than the 4 MHz fundamental beam. The harmonic beam has significantly
Iower sidelobes than both fundamental bearns. Both these qualities afTord harmonie imagîng
improved lateral resolution over conventional imaging. Wojcik et al. (1998) fùrther cal-
cuiated the nonlinear beam after aberration caused by a realistic mode1 of abdominal wall
sections, and dernonstrated that not oniy does the improved lateral resolution ca ry over
to an attenuating and aberrating situation, but that haxmonic beams &O d e r less from
CHAPTER 1. INTRODUCTION 31
the image quality degrading effects of phase aberration. It has now been demonstrated that
hazmonic imaging without contrast agent, c d e d tissue harmonic imaging, provides some
compensation for the image degradation caused by gas pockets and fat and connective tissue
layers (Burns et al. 2000; Sranquart et al. 1999).
O 0.1 0.2 0.9 0.4 0.5 0.6 0.7 0.8 0.9 1 RADIAL DISTANCE (cm)
Figure 1.9: Calculated transverse beam profiles on the focal plane showing 2 MHz fundamental
(solid), 4 MHz fundamental (dots), and 4 MHz second hanrionics Rom the 2 MHz beum
(dadies). All curues were nonnalized. Reproduced from Chnstopher (1997).
1.5 Thesis Outline
The goal of this thesis is to develop a theoretical model for the acoustic response of mi-
crobubble contrast agents in the context of dtrasound imaging applications.
In Chapter 2, a theoretic mode1 is developed which incorporates bubbles of various
sizes placed in a heterogenous ultrasound field. This population ensemble model was created
to addreçs the most important deficiencies of the single bubble model, which begins with the
observation that single bubbie models respond to only narrow ranges of frequencies while
experimentdy, contrast agents have a very broadband response.
In Chapter 3, an experiment was designed to test quantitatively the preàicting power
of the population ensemble model. The results of this experiment demonstrated the general
validity of the model, however, some quantitative discrepancies were identified.
In Chapter 4, possible explanations of the discrepancies were considered and shell
effects were identified as a probable source of the error. An experiment was designed to test
the hypothesis that damping by the shell and acoustic disruption of the shell can be the
cause of the observed dXerence between theory and euperiment. The results demonstrated
that such is indeed the case, and the shell effect was discovered to be surpcisingly important
in single scattering.
In Chapter 5, recent developments in nonlinear contrast imaging are recounted. Some
of these developments raise questions that can be answered with the help of the microbubble
scattering model. Applications of the model in these contexts are presented.
A swnmary of the thesis and future directions for the scattering model c m be found
in Chapter 6.
Chapter 2
A Population Mode1 of Contrast
Microbubbles
Although the behaviour of a bubble in an acoustic field has been studied ertensively, few
theoretical treatments to date have been applied to simulate the acoustic response of a real
population of variabiy sized microbubbles in a finite width sound beam. In this paper,
we present a modined Triilhg equation for single bubble dynamics which has been solved
numerically for different conditions. Radiated waveforms fiom a large number of such bubbles
are combined, reflecting thek size distribution and Location and the shape of a red acoustic
beam. The resulting time-domain pressure waveforms can be compared with those obtained
IThis chapter was based on the pape.: Chin CT, Burns PN. Predicting the acoustic re- sponse of a microbnbble popdation for contra& b g k g in medical ultrasound. Ultrasotand Med Bi01 2000;26:1289-1296.
CHAPTER 2. A POPULATION MODEL OF CONTMST MICROBUBBLES 34
experimentally. The dependence of second h m o n i c radiation on incident focal amplitude at
different fiequencies is presented. This mode1 is particularly suited to the study of interaction
between a medical ultrasound beam and microbubble contrast agents in aqueous media.
2.1 Introduction
Microbubble suspensions for use a s contrast agents in medical ultrasound imaging are cur-
rently undergoing àgnificant development. When these bubbles are e-xposed to moderately
strong (> 100 kPa) ultrasound waves, they exhibit nonlineu radial oscillation and produce
echoes containing second and higher harmonies of the incident wave. The second harmonic
emissions can be used to distinguish blood from tissue echoes and form the basis of such new
methods as harmonic (Burns et al. 1996) and pulse inversion imaging (Hope Simpson et al.
1999).
Most of the research so far has been focused on empirical measurements of various
parameters of contrast agents in vitro and an vivo. Few theoretical studies have been aimed
at simulating actuai imaging conditions. The earliest studies were aimed at understanding
coIIapse of a bubble due to turbulent flows and undemater explosions (Rayleigh 1917; Plesset
1949). In such studies, the cavity collapses freely without ex temdy applied sound waves.
Another class of studies focuses on the steady state response of a bubble to (nearly) contin-
uous incident sound waves. For these, the cornplete differential equation can be lùieaized
by using the s m d amplitude approximation. Using suitable ünearization, the amplitude
and phase of the fundamental and second harmonie component can be calculated (Leighton
1997; Miller 1981). A third class of studies investigated the dynamics of a bubble in the
field generated by a üthotripter (Church 1989). In this situation, resonant oscilIation is in-
significant and gas diffusion into the bubble is the most important process. In this paper,
we present a theory for predicting acoustic response of a bubble population for diagnostic
contrast imaging.
Mathematicdy, a model of spherical bubble oscillations can be understood as a basic
differential equation that describes the BOW of the üquid outside of the bubble, and a set
of boundary conditions and correction terms that describe the gas pressure, surface tension,
liquid viscosity and damping mechanisms. The basic diaerential equation has three cornmon
forms. Rayleigh (1917) originally derived an equation to calculate the collapse of a spherical
cavity in an incompressible liquid. Subsequent authors (Hemng 1941; Keller and Miksis
1980; Trilling 1952) allowed a compressible liquid which mpports linear acoustic waves to
propagate at a finite constant speed. Currently, the most sophisticated form of the basic
equation was derived by Gilmore (Akuiichev et al. 1968; Hickling and Plesset 1964; Gilmore
1952), who took into account nonlinear propagation caused by the convective component of
the Navier-S t okes equat ion and the noniinear compressibility of water .
The Rayleigh formulation, with some important modifications by Plesset (l949),
Devin (1959) and EIler (1970), is the most well known and has the advantage of being
intuitive. This form is most commonly used in studies in bubble emboii (Eatock and Nishi
1985) and contrast agents (de Jong et al. 1994). It has been demonstrated that, when the
speed of the bubble boundary reaches a significant fraction of the speed of sound in wa-
ter, Herring's and Gilmore's formulations are significmtly more accurate than the Rayleigh
CHAPTER 2. A POPULATION MODEL OF CONTRAST ~ ~ O B U B B L E S 36
model (Vokurka 1986). An acoustic or radiative damping term was used as a modification
to linearized versions of the Rayleigh model (Devin 1959); however, such terms explicitly in-
clude the fiequency of bubble motion and are inappropriate for nonsinusoidd or broadband
motions-
There are three key components to the proposed model. Firstly, the dynamics of the
radial motion of a bubble were simulated by integrating numerically an equation similar to
one used by Trilling (1952). The Rayleigh formulation has been most widely used to model
single bubble responses for medical ultrasound contrast agents, usually with continuous wave
excitation (de Jong et al. 1994). Bubble response (such as resonant frequency and scattering
cross-sect ion) t O short pulse incident wave can deviate significant ly from cont inuous wave
response; thus, it is important to use the same incident wave in both theory and experiment.
By using a mode1 which treats the liquid phase more realistically and by considering short
pulse excitation, we improve the theoretical framework for the calculation of a single bubble
response.
Secondly, as red agents contain bubbles with a range of radii, simulation at any single
bubble size cannot be accurate, especidy over a range of Frequencies. Our model contains
an ensemble of unencapsulated bubbles with a size distribution based on that of an actual
contrast agent, OptisonTM (Mallinckrodt Inc, St . Louis, USA).
Finally, coherent interference of the scattered signal kom multiple s m d targets causes
amplitude fluctuations in the detected echo. This process is, in principle, the same as that
which produces the tissue speckle which characterizes parenchpal textures in medical ultra-
sound images. However, as the bubble response depends nonlinearly on incident amplitude,
the speckle formation process becomes nonlinear aho. In particular, the amount of hannonic
emitted may be iduenced by the beam shape. In our model, a bubble located away from
the beam center contributes a pulse with a different waveform to that fiom one located at
the center, due to the clifference in local incident pressure amplitude.
2.2 Theory
2.2.1 Single bubble
Triiling's (1952) original derivation of the single bubble theory has been modified for two
reasons: (1) m g ' s problem was that of a bubble collapsing in a othenvise undisturbed
liquid, while we are studying a stable bubble in a sound field; (2) the original equations
were cast into an approximate form for a stegwise method appropriate for the limited
computation resources of the time. We have rederived the equations into a more direct form
and removed some approximations no longer necessary in the age of high-speed computers.
Since the bubble radius R is mal1 compared to the wavelength, the incident propa-
gating wave can be described by a spatidy-uniform pressure, p, (t). The system is assumed
to be isotropie and irrotational, allowing a velocity potentid # to be defined as u = &5/&.
Trilling's assumption was that acoustic wave propagation is linear, implying the equation of
da te to be dp = clp/& This is accurate to the order of ulc. Surface tension and viscosity of
the liquid are included. Mass t r a d e r across the bubble boundary is assumed to be insignif-
icant over the time duration of interest, which is typically l e s than 10 p. The polytropic
assumption, which states that the interna1 gas pressure is given by p~ ( & / R ) ~ ~ , where pgo
CEIAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES 38
is the equiiibrium gas pressure, l& the equiiibrium radius, and K a polytropic constant, is
used.
The theory begins with the conservation of momentum for the üquid phase:
Integrating from a point r to w, assuming 4 = O and u = O at r = w produces:
To obtain the desired result, one needs to rearrange equation (2.2) to relate the state at the
boundary R with the incident pressure at infinity. Intermediate terms involving 4, u and p
are to be expressed in terms of velocity of the bubble boundary U (= k) and the pressure
just outside the bubble boundary P(t ) (= p(R(t), t ) ) .
To eliminate a+/ût, we recail the ünear wave equation for outgoing sphencal waves:
where p and c are the iiquid density and speed of sound, respectively. Dserentiating both
equations (2.2) and (2.3) with respect to t, and rearranging, we have:
CHAPTER 2. A POPULATION MODEL OF CONTRAST MZ%ROBUBBLES 39
We seek to evaluate equation (2.4) at r = R. To eliminate &/%IR and a p / û t l R v we
can use four h e a r equations to solve for four quantities (dîl/atlRt ûplâtl,, &/&I and
&/&IR). Three of these equations are equation (2.1) and the expressions for dU/dt and
dR/dt in t e m s of partial derivatives of u and p with respect to t and r. The last equation
arises kom conservation of mas:
in which the terms involving p are replaced by p through the equation of state. Substituting
the results into equation (2.4), and using the equation of state to evaluate the integral J d p l p ,
we obtain h d y the equation for the motion of the bubble boundary:
It is noted that equation (2.6) can be simpued somewhat by a few approximations. The
term is typicdIy mal1 compared to unity, and the logarithmic term on the right hand
side of equation (2.6) can also be simpüfied. In the iimits P < pot? and p, < p o 2 ,
CHAPTEIR 2. A POPULATION MODEL OF CONTRAST MICROBOBBLES
Therefore, equation (2.6) becomes
Equation (2.7) is equilivalent to (2.6) to the order of U2/c? (and as long as the minimum
bubble radius is greater than 10% of the initial radius), and it is the form published by
Trilling (1952) and Vokurka (1986).
The pressure at the bubble boundary P is given by
where p is the viscosity of water and a is the surface tension. The form for viscous damping
was derived by Pontsky (1951) which, unlike the linearized darnping term introduced by
Devin (1959), is suitable for nonsinusoida1 motion. There are two approaches to account for
thermal damping. Devin (1959) and Eller (1970) derived a Iineaxized darnping term by as-
suming a s m d sinusoidal oscillation. Their damping term includes explicitly the frequency
of the bubble motion and can not be converted ~ ~ O U ~ O U S ~ Y into a form for wideband m e
tions. To account for nonperiodic motions of excited bubbles, Prosperetti (1991) developed
a therrnd behaviour mode1 in which the gas component is assumed to have a unifonn pres-
sure but the gas temperature varies spatially. The result is a partial differential equation For
the gas temperature as a function of t h e and radius. The partial differentiai equation is
conpled with equation (2.6) and can increase the computation load by orders of magnitude.
Chapman and PIesset (19?1), using a linearized approach, estimated that thermal damping
CHMTER 2. A POPULAïTON MODEL OF CONTRAST lMICROBUBBLES 41
for a 2-pn air bubble in water represents about 25% of total damping and is about equal
to half the viscous damping. However, their calcdation also showed that viscous damping
and thermal damping have very different dependence on the bubble size, making it unadvis-
able to model thermal damping a s an additional viscous tem, a rather tempting notion at
hst sight. Unfortunately between the Iineaxized approach and the hl1 approach there has
not been a verified method to model the thermal damping that can be justifiably applied
to a wideband rnildly-nonlinear model. In this thesis, the effect of thermal damping is not
included.
Now equations (2.6) and (2.8) can be solved numericdly to give the time-course of the
bubble radius R(t). The velocity potential $ (r, t) throughout the liquid cm be calculated
from equation (2.2) as
Equation (2.9) satisfies the wave equation (2.3) by Wtue of being of the form f (t - r /c ) / r .
The pressure can then be calculated from equation (2.2):
PS' SY - for r » X
r
where f ' (x ) = df (z)/dx. Equations (2.6), (2.9) and (2.10) differ somewhat from Trilling's
(1952), suice he considered oniy the case p, = O and approximated the logarithmic terms
C W T E R 2. A POPULATION MODEIX OF CONTRAST MICROBUBBLES
to the form (P - p,)/p&
2.2.2 Secondary scattering
Before the response of a population of bubbles c m be calculated, it must be ascertained that
one bubble's scattered ultrasound wave does not interfere with the scattering process of its
neighbours, in another word, secondary scattering is insignificant. The ratio of pcimary to
secondary scattering is equal to the ratio of the incident intensity to the p n m q scattering.
This secondary scattering ratio is therefore given by o,/r2, where os is the (primary) scat-
tering cross-section and r is the distance between neighbouring bubbles. ResuIts from single
bubble calculatioos show that the maximum scattering cross-section at 1-10 MHz is of the
order of 10-Iom2. The distance between neighbouring bubbles is calculated next.
In analogy to molecules in an ideal gas, it is assumed that the bubble density is
sufnciently low that bubbles rarely corne into contact and that each bubble exerts no force
on each other. The position of each bubble is then cornpletely independent of each other.
The probability that x bubbles are Found within a volume V is then @en by the Poisson
distribution:
where N is the average number of bubbles per unit volume. For any given bubble, the
probability density function of the distance to its nearest neighbour r is written as f (r),
çuch that f (r)dr is the probability that the nearest neighbour is at a distance between r and
CHAPTER 2. A POPULATION MODEL OF CONTRAST hIICROBUBBLES 43
r + dr. To calculate f (T ) , consider a coordinate system with its ongin at the position of an
arbitrary bubble. Since the presence of this bubble at the (fixed) origin does not influence
the positions of al1 the other bubbles, it can be removed from our consideration without loss
of generality. Cleady then, f (r)dr is equal to the probability that there are no bubbIes inside
the sphere with radius r and that there is a single bubble inside the spherical shell between
T and r + dr. Therefore,
.In 3 where V = and dV = 4*rzdr. Expanding e-NdV as a series and then dropping al1 terms
of (dl / )2 and higher orders from equation (2.12), one obtains
- ~ , J N f ( r ) = 4 ? r r 2 ~ e 3
-4 distance unit r, can be dehed as Jr: = 1/N, equation (2.13) then becomes
Note that r, is not the mean distance between a bubble and its nearest neighbour, integrating
J r f (r)dr, one obtains the mean distance between a bubble and its nearest neighbour to be
0 . 8 9 3 0 ~ ~ = 0.5540~-' '~.
Using Optison as an example, the maximum in vivo concentration is about 0.196,
this gives N = 5 x 10~ml-'. Therefore, on average, the secondary scattering ratio is 2%.
CHilPTER 2. A POPULATION MODEL OF CONTRAST MTCROBUBBLES 44
Note that this value is sigxdicantly over-estimated since the value of N for all bubble sizes
was used. In reaüty, only a small fraction ( les than 1%) of bubbles have os = 10-~Orn?
Asniming 1% of the bubbles are resonant (os = 10-Lom2), the average secondary scattering
ratio drops to 0.4%. It is also interesthg to consider the probability of significant secondary
scattering. If a secondsry scattering ratio of 10% is defined as significant, two bubbles has
to be less than 31 pm apaxt. The probability that a resonant bubble fin& another resonant
bubble within 31 pm is calculated from equation (2.14) to be 1.1%. With these results, one
can calculate, with confidence, the scattering from a bubble population by sumrning linearly
the scattered wave from each individu4 bubbles.
2.2.3 Echoes from suspensions of bubbles
We now mode1 a randorn suspension of N bubtles exhibiting the motion described above.
The i-th bubble has random radius RE and radial and axial positions and zi as shown in
figure 2.1. The axial length of the sampled volume need only be as long as the duration of
the longest bubble echo in order for the echo properly to be calculated. The single bubble
echo is estimated conservatively to be at most four times as long as the incident pulse. For
typical imaging pulses of l e s than eight cycles, it follows bubbles more than 32 wavelengths
apart do not contribute interferhg echoes; therefore, the sample volume is short cornpared *
to the focal depth of typical imaging beams, dowing us to approximate the beam to be
Wilfom in the auid direction. .4ssuming the minimum f-number (focal lengthlaperture) of
an imaging beam to be 3, which gives a -6 dB depth-of-focus of 63 wavelengths, the enor in
assnming an & d y d o m beam is l e s than 7.5% or 0.7 dB.
Radiated Bubbles 2"' Harmonic
Radiated a Fundamental
To Receive \ Sarnple Volume
Transducer
Figure 2.1: Each bubble in the sample volume contributes a diflerent wavefonn to the final
signal depending on its size and local incident amplitude.
The incident pressure wavefom for the i-th bub ble is given by p, (t) = A. B (ai) Pin(t)
where ilo is the peak-to-peak focal pressure amplitude, B(a) is the normalized beam profile
and Pi,,(t) is the normalized pressure wavefonn. The radiated pressure wavefonns calculated
f m equation (2.10) were scaled by B(%) and time-shifted according to and summed to
give a the-domain echo from the bubble ensemble.
2.3 Results and Discussion
2.3.1 Single bubble mode1
The single bubbIe mode1 was numerically solved with a third order Runge-Kutta method for
a range of bubble radii l& fiom 1 to 15 pm and a range of peak amplitudes A. between 1
kPa and 1 MPa for each normalized incident wavefonn P*(t). Air bubbles in water were
CHAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES 46
considered, using parameted listed in table 2.1. The transmitted waveform used was based
on that recorded with a hydrophone frorn a focused disk transducer. The transducer was
excited with a 2.9 MHz, two-cycle pulse fiom an arbitrary waveform generator. The reason
this pulse was chosen was that it is M a r to pulses used in clinical scanners and identical
to pulses used in ongoing benchtop contrast agent experirnents. Figure 2.2 shows t b
and fiequency- domain plots of Ph(t). In reality, when the peak amplitude approaches 1
MPa, nonlinear propagation generates a second hamnonic field, which, in a mildly nonlinear
nearly lossless medium such a s water, c m reach -15 dB relative to the fundamental field.
This second hannonic field contributes to the nonlinear components in the signal scattereci
by the bubbles. However, the relative contribution of the propagation h m o n i c s in the
scattered signal is not immediately predictable. Both the magnitude and the phase angle of
the harmonic component in the transmitted field have a signincant effect on the scattered
harmonic (Urnemura et al. 1996). Furthemore, due to the uncertainty of the in vivo
nonlinear parameter and attenuation, the magnitude of the haxmonic field is unpredictable
even when the fundamentai field is to some extent estimable. Therefore, it is a t this point
TabIe 2.1: Paranzefers vsed in the numerical calculatzon.
Value 988 kg-m-3
0.0725 N-m-' 0.0009 Pa sec 101325 Pa
Parameter Water density
Surface tension Water viscosity
Ambient pressure Polytropic constant
S ~ e e d of sound in water
*The equilibrium gas pressure p~ is not a fixed parameter and is instead determined from the ambient pressne po, eqrrilibrium r a b & and d a c e tension a.
Variable P O
P PO K;
c 1.33 1481 msec-'
CHAPTER 2. A POPULATION MODEL OF CONTMST RUCROBUBBLES
1 2 3 4 5 O 3 6 9 Time (p) Frequency (MHz)
Figure 2.2: Measured transmitted pulse vsed for simulation.
more instructive to study the bubble population response to undistorted incident waves.
Since the presently proposed method is a time-domain method, the effects of nonlinearly
propagated incident waves can easily be studied.
Figure 2.3 illustrates four typical responses in radius change and radiated pressure.
In figure 2.3a, a srnail bubble (2% = 1.2 pm) which has a resonant frequency (5.3 MHz)
much higher than that of the incident pulse radiates only weakly (0.1 Pa when driven by
5.0 'Pa). Similady, a large bubble (2& = 6pm) with a low resonant frequency (1.1 MHz)
radiates at a simila amplitude but with reverse phase (figure 2.3b). A 3.0 pm bubble (2.8
M H z ) , on the other hand, radiates 10 times more strongly (figure 2.3~). However, when the
incident ampütude is increased to 100 kPa, the motion becomes nonlinear and signincaat
distortion appears in the echo (figure 2.3d).
For each incident pulse Pk(t), severd hundred responses For Merent bubble sizes and
CHAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES 48
O 2 4 6 Time us)
O 2 4 6 Time @)
Figure 2.3: Four types of c u h l a t e d response to the two-cycle wave, in t e m of radius change
(ieft) and radtated pressure (right) at 40 mm. (a), (b) and (c) Responses of 1.2 Pm, 6.0 pm
and 3.0 pm diameter bubbles to 5 kPa peak-to-peak incident amplitude. (d) Response of the
3.0 pm bubble to 100 kPa inczdent amplitude.
incident amplitudes were generated. To reduce calculation time without sacnficing accuracy,
irregular samphg of bubble sizes was used. The large quantity of data can be visuaüzed
quickly by distilling some quantities of interest fiom the wavefoms and displayhg them as
maps. For h m o n i c irnaging, these quantities are the fundamental and second harmonic
cross-sections. Cross-section is defined as the total radiated power within a frequency band
divided by the incident intensity. Figure 2.4 shows maps of these cross-sections. One sees
that the fundamental cross-section shows a strong resonance at about 3.0 prn diameter and
the response is essentially independent of incident amplitude up to about 100 kPa. Above
100 kPa, nonlinear effects set in to broaden the response, reduce the resonant size and reduce
the peak crosssection. The reduction of fundamental crosssection is due to a transfer of
energy to higher hamionin. Thus, in the second h m o n i c cross-section, one can see a
gradual increase towards a maximum at about 500 kPa frorn the same resonant bubbles.
Near 1 MPa, so much energy is transferred to the higher harmonies that even the second
harmonic cross-section is reduced.
These maps produce useful insight into the interaction between bubble nonlinearity
and beam shape. For safety reasons, regdatory agencies require the spatial peak pressure
of each scanner to be measured and reported in tems of MI. However, most of the bubbles
in the imaged volume are insonated at amplitudes lower than that implied by the displayed
MI. The fiaction of bubbles exposed to merent incident amplitudes is a function of the
beam profle. Therefore, a spatial average of incident amplitude would be a more sensible
measwement than MI when contrast performance between different machines or different
imaging modes is compared.
C W T E R 2. A POPULATION MODEL OF CONTRAST MlCROBUBBLES
2 4 6 8 Bubble radios Ro (pm)
O 2 4 6 8 Bubble radius R, (un)
Figure 2.4: Caleulat ed fundamental (top) and second harmonzc (hottom) cross-sections (in
ma) of single bubbles to Pi,,@). The grey leuel represents lznearly the cross-sectional areas.
The tick marks dong the top and nght edges of the figures mark the exact radiz and amplitudes
of euch calculation.
CHAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES 51
Another consequence is the effective sidelobe suppression that harmonie irnaging offen
under certain conditions. For example, if the amplitude is 300 kPa at the focus and 60 kPa at
the highest sidelobe, then figure 2.4 suggests that the bubbles in the sidelobe will contribute a
Eractionally smaller amount of energy to the h m o n i c signal than to the Fundamental signal.
Similady, bubbles at the rim of the main lobe contribute l e s to the total harmonic signal.
Thus, h m o n i c imaging &ers less from sidelobe artifacts and has sharper laterd resolution.
These effects help to explain why harmonie imaging produces high quality images despite
its lower axial resolution compared to conventional imaging. The mechanism is related to
the image quality improvement seen in tissue harmonic imaging which relies on nonlinear
propagation of ultrasound pulses (Christopher 1997; Ward et al. 1997) (see also section
1.4.3).
2.3.2 Prediction of population response
The distribution of bubble radii, &, in our ensemble is based on that of OptisonTL1 (Skyba
et al. 1996) and is plotted in figure 2.5a. Due to the Limitations of optical sizing equipment
using visible Iight (wavelength = 0.4-0.6 pm), measmement of bubbles smaller t han 1.0 pm
is not available. -4 total of about 1400 simulated bubbles were used in a sample volume
of 10 mm radius (a) and 7.5 mm thickness (z ) , corresponding to a concentration of 1 pl/l.
T m - t w o independent randorn ensembles were used to estimate the standard error of the
caldated values. The beam profile B(a), recorded eom hydrophone measurements, is
plotted in figure 2.5b. Time-domain echoes were calculated at a range of incident focal
peak-to-peak amplitudes Ao. To understand further the dependence on frequency, the whole
CHAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES 52
calculation (starting from single bubbles) was repeated for two additional incident waveforms
at about 1.4 and 5.8 MHz. These waveforms were generated by cornpressing and dilating in
time the transmitted puise in figure 2.2.
1
O 10 20 -10 O 10 Bubble Diameter (2RJ (pm) Axial Distance (a) (mm)
Figure 2.5: (a) Measured szze distribution of bubble ensemble. (6) Measvred transdvcer beam
profile B(a) used in calculation of agent response.
Second and higher harmonies were found in the the-domain echoes, as reveded by
Fourier andysis. The normalized spectra for 2.9 MHz incident frequency at different incident
amplitudes are plotted as a map in figure 2.6. The spectra were normalized by dividing by
the square of the incident amplitude. Up to the sixth harmonie can be seen. One can observe
that the h m o n i c peaks were broadened at higher incident amplitude, to the extent that
at 1 blPa (a typicd diagnostic imaging peak pressure) the spectnun is ahos t completely
smeared out, leaving the fundamental peak b a d y distinguishable from the harmonies.
O 3 6 9 12 15 18 Frequency (MHz)
Figure 2.6: Nonndized Fourier spectra of the simulated bulk agent echoes. The spectra were
nonnalized by dividing by the square of the incident amplitude. The grey level represents dB
scale. Notice spectral bmadening of the harmonzc peaks at high inczdent amplitudes.
The powers at the position of the receiving transducer at fundamental and second
haxmonic frequencies were calculated and plotted in figure 2.7. The power radiated drops
by almoût a factor of 100 between 1.4 and 5.8 MHz. This fiequency dependence for buk
contrast agent has been demonstrated by experiment (de Jong and Hoff 1993). The negative
freqnency dependence can be explained thus: whüe there are many more s m d bubbles (0.5
- 2.0 p) in rnost agents, the scattering cross-section at resonance of the individual bubbles
demeases more quickly with decreasing bubble size (and inmeasing frequency), so that the
CHAPTER 2. A POPULATION MODEL, OF CONTRAST MICROBUBBLES 54
combined effect is a negative dependence. In the fundamentai band, the power received is
approximately proportional to the square of the incident amplitude. The power exponent
was measured to be 2.1 izO.15 for A. < 100 kPa, and gradudy decreases to l .7f 0.3 between
100 kPa and 1 MPa. In the harmonic band, the maximum power exponent for 2.9 MHz and
5.8 MHz is about 3.75 & 0.15 and decreases to about 2.8 10 .3 at incident amplitudes above
100 kPa. But at 1.4 MHz, the maximum siope reached only about 3.0 at 200 kPa. At both
fundamental and second harmonie, responses at all frequencies show a saturation effect above
100-200 kPa. While these results were calculated for a focused disk transducer, qualitatively
similar results can be expected for other common transducer geornetries, including arrays.
Presently, the accuracy of the model is limited by the lack of a thermal model and a shell
model. Thermal damping is expected to reduce the total scattered amplitude and degree
of nonlinearity. The shell can be expected to increase damping and increase the resonant
fiequency. The accuracy of the model is also limited by an uncertainty in some physical
parameters such as shell thickness, material properties, in vivo size distribution and local
incident amplitude.
2.4 Conclusions
We have developed a new model of contrast agent response to a real ultrasound beam.
Individual free bubble responses to pulsed incident waves were calculated numerically from a
differential equation çimiIar to 'Ililluig's (1952). Maps of bubble response properties, such as
fundamental and harmonic scattering cross-sections, can provide insïght into the interaction
CHAPTER 2. A POPULATION MODEL OF CONTRAST MICROBUBBLES
1.4 MHz * . . . . . 2-9 MHz 5.8 MHz
+ I * 1
Incident Peak-ta-Peak Amplitude A, (Pa)
1 0' 10' 106 Incident Peak-*Peak Amplitude A, (Pa)
Figure 2 . 7 Fundamental (top) and second hannonzc (bottom) responses of szmuZated agent as
a fvnction of zncident focal amplitudes ut three Fequencies. The error bars zndicate standad
m o r of 32 simulateci ensembles.
A POPULATION MODEL OF CONTRAST MICROBUBBLES
between bubble size and incident ampIitudes, which in tuni provide a possible exphnation
of reduced sidelobe ghosts and Mproved lateral resolution of h m o n i c imaging. A large
number of single bubble responses were combined to produce radio fkequency tirne-domain
echoes that redisticdy reflect the distribution of bubble sizes and the non-uniformity of the
incident and receive beams. This makes the single bubble theory experimentdy verifiable
as a method for predicting bdk agent acoustic response in Mtro and in vivo. In particular,
the model predicts a smearing of the fundamental and harmonic responses at high incident
pressures. As hannonics Erom tissue echoes due to nonlinear propagation do not show the
same effect, this may have important consequences for strategies to separate tissue and
bubble echoes. An experiment designed to test the quantitative accuracy of this model is
presented in the next chapter.
Chapter 3
Experimental Verification
Abstract l
A t heoreticd contrast agent model, extending existing single bubble models to a population
of simulated bubbles, was previously reported to produce time-domain scattered signals of
a form comparable to those obtained from a diagnostic imaging systern. In this paper,
experiments were camied out to test this model quantitatively. A diluted suspension of
contrast agent microbubbles Bowing in a chamber was exposed to 5 MHz pulsed ultrasound
of various bandwidths. Scattered signais were detected at 90° by a broadband transducer.
The experirnent a1 results generdy c o n h our model for predict ing scatt ered signds, but
the measured second hamtonic scattering is up to 10 dB lower than the theoretical prediction.
It was also observed that scattering is hcreased at hi& transmitted amplitude (> 1.5 MPa).
'This chapter is based on the manuscript: Chin CT and Burns PN. Experimental ver& cation of an ensemble model for scattering by a population of contrast agent microbubbles. Uitrasound Med Bi01 (submitted) .
Sheli disruption is believed to be a possible cause for both effects, and it is proposed that
the sheU behaviour is significsnt in determinhg the acoustic reponse of contrast agents.
Introduction
Microbubble suspensions for use as contrast agents in medical ultrasound imaging are cur-
rently undergoing signifiant development . Most of the successful contrast imaging met hods
exploit the phenornenon of nonlinesr scattering of ultrasound by the microbubbles. However,
quantitative understanding of nonlinear scattering is still poor.
The most successful quantitative measurements of ultrasonic characteristics of con-
trast agents have been performed using continuous waves (CW) at low (often unspecified)
transmitted amplitudes. Bleeker et al. (1990) established that, at low concentration, at-
tenuation and backscatter are approxirnately linearly related to the number of Albunex
microspheres. de Joug et al. (1992, 1993) measured the attenuation and scattered power of
Albunex over a frequency range of 1-10 MHz and found them to agree well with a linear
model based on visco-elastic particles. Hoff and Sontum (1998) reported at tenuat ion spectra
of the contrast agent NClOOlOO to agree with a similar model. Marsh et al. (1988) found
excellent agreement between measured t r e o n and backscatter spectra and prediction
fiom a h e m model.
A number of studies have been directed at quantitative measurements of the second
harmonic scattering of contrast agents. de Jong (1994) measured the second harmonic corn-
ponent generated when ten-cycle bursts propagate through a sample of diIuted Mbunex at
low (25 kPa and 50 kPa) tranmitted ampiitude. Uhlendorf and Hoffman (1994) reported
that the relative second harmonic output of SHU563A (Sonavist), in response to 35-cycle
bursts, increased by more than 30 dB when the incident amplitude was increased Erom 25
kPa to 400 kPa. Using 10-cycle bwsts, Krishna and Newhouse (1997) reported a quadratic
dependence of second harmonic scattering of Albunex on transmitted amplitude; a more
complicated dependence was found Eor FS069 (Optison). SUnilarly, using a CW Doppler
technique, Chang (1996) found that, for incident amplitudes below 80 kPa, Mbunex and
Optison produced a second harmonic amplitude in approximate proportion to the second
power of the transmitted amplitude. The quadratic dependence, used by many of the authors
cited, was derived originally by Miller (1981), who used a power series expansion technique
on the Rayleigh-Plesset model. When only the first nonlinear term was retained, a quadratic
dependence was the r e d t . Such a technique was intended for weakly nonlinear oscillation
and becomes invalid when the amplitude of the radial motion reaches a significant Fraction
of the initial radius. We now know that in diagnostic ultrasound contrast imaging, radid
excursions of five times the radius is possible (Dayton et al. 1999).
To help understand the nonlinear scattering of contrast agents, a theoretical mode1
was developed to predict the acoustic response of a population of microbubbles to pulsed
ultrasound such as that used in diagnostic imaging as described in Chapter 2. It was proposed
that to account for the basic nonlinear behaviour of contrast agents, it is necessary to consider
a randody distributed ensemble of bubbles with a range of bubble sizes. Cdculatioos using
this model have demonstrated a signiscant difference to the power series approximation
(Hope Simpson et al. 1999).
One specific prediction made by the model is the spectral broadening of radio fie-
quency (RF) echoes at high transmitted amplitudes, which codd potentidy be used to
address a problem with harmonic contrast imaging. Hmonics produced by nonlinear
propagation in solid tissue compete with harmonies produced by nonlinear scattering by
microbubbles and limit the performance of second harmonic imaging. Since nonlinear prop-
agation does not produce spectral broadening, techniques that exploit the scattered signal
a t 1.5 times the transmitted frequency could be used to distinguish between solid tissue and
blood Bow signals. To test the validity of the rnodel, h e a r and nonlinear scattering of pulsed
ultrasound kom diluted Definity (Dupont Pharmaceuticals, Wilmington, DE) was measured
and compared to the results of numerical simulation.
3.2 Method
IdealIy, with a multi-step model, one would like to verifjr evperirnentally each of the indi-
vidud steps. However, experimentd verification of the single bubble rnodel is difficult. The
microbubbles themselves are fragile and often axe destroyed before they can be selected and
manipulated into the sensitive volume of an experimentd system. Consequently when sig-
nais are detected fiom a single bubble, there is significant uncertainty in both the size and
position of the detected bubble. Thus, its value as a cnticd quantitative test of the accuracy
of the single bubble model is limited. Therefore, the complete population mode1 was tested
by measnring the scattering properties of population of bubbles at a cünical concentration.
Definity diluted to 0.075% was use&
The experimental setup, as shown in figure 3.1, employed separate transmit and re-
ceive tramducers at right angles to each other. This design has the important advantage
over the single transducer pulse-echo experiment in that the nodinear circuit elernents such
as diode-based expanders and Iimitea are eliminated.
Contrast Agent
Waveform 1 l b Generator -.-J 250 MHz .*.: I \
6.5 MHz Transducer
Signal Amp.
40MHz8bits 1-165MHr 0-20 d 8 Digitizing C' Bp Filter Attenuator
Oscilloscope
Figue 3.1: Eqerïmental setup for the nonlznear scattering memurement.
A Sony/Tektronix (Beaverton, OR) AWG2020 250 MHz arbitrary waveform genera-
tor was programmed to produce Gaussian enveloped pulses centred at 5.0 MHz with two
different bandwidths (figure 3.2), which were then amplined by an ENI (Rochester, NY)
240L 50 dB power amplifier. A Matec (Northborough, MA) 5.0 MHz transducer (aperture
f/2, focal Length = 19 mm) was used to produce ultrasound pulses that propagate into a flow
ceII which has mylar membranes as acoustic windows. The distance between the transmit-
ting transducer and the sample m1ume was kept short to reduce propagation nonhearity.
The scattered ultrasound was detected by a Blatek (CoUege Park, PA) 6.5 MHz transducer
(aperture f/4, focal length = 38 mm) at 90°. The signal was attenuated with a Te-
(Indianapolis, IN) variable attenuator (necessary at high transmitted amplitudes) and then
amplified by a Miteq (Hauppauge, NY) 50 dB signal amplifier. The amplified signal was
then fiitered with a custom 1-16.5 MHz bandpass filter to remove noise and digitized at 40
MHz with &bit resolution using a LeCroy (Chestnut Ridge, NY) 7200 digital oscilloscope.
The transmitted pulses used in the calculation were meanired with a calibrated hydrophone
(Sonic Technologies, Hatboro, PA). The bubble size distribution and beam shapes of both
transmit and receive transducers were obtained fiom experimental measurements and are
displayed in figure 3.3. The size distribution of Optison was used here. Definity may have
more sub-micron bubbles than Optison, but over the narrow range of frequencies used in this
study (conespondhg to 1.6-1.9 pm), the number density is very similar between Defintiy
and Optison. Due to the limitations of optical sizing equipment using visible light (wave-
length = 0.4-0.6 pm), measurement of bubbles srnaller than 0.5 Pm (radius) is not available.
The power spectra of the calculated ensemble response (using equations 2.6 and 2.8) are
plotted in figure 3.4.
This setup effectively eüminated interference lrom direct acoustic coupling or solid
structure reflection, dowing measurements at transmit pressures below 70 Wa. The second
harmonic component of the transmitted beam due to nonlinear propagation in water was
measured with the Sonic Technologies hydrophone. At the matcimm transmitted amplitude
of 3.8 MPa, the second h m o n i c component was 22 dB below the hindamental. However,
during the experiment, a portion (7 mm) of the beam path (19 mm in total) was within the
sample ceiI. Since the diluted agent has a higher nonlinear parameter, the actual propagation
harmonic rnay be higher.
O 5 10 15 Freq. (MHz)
O 5 10 15 Freq. ( M H z )
Figure 3.2: ICfansmitted four- y c f e (Ieft) and one-cycle (right) w a v e f o m and the correspond-
h g frequency spectrurn (bottom) wed in both simulation and ezperiment.
Since bubble echoes are known to decay in a manner that depends on ultrasound
amplitude (Burns et al. 1994), it was decided that data would only be collected from bubbles
that were never exposed. This was accompüshed by employing a very low pulse repetition
kequency (Pm) of 8 Hz and by Bowing the diluted Defhity through the Bow cell. Flow
velocity in the fiow cell was measured separately to ensure complete refreshrnent of contrast
bubbles between pulses. To prevent agitation and flow-induced bubbles from contamioating
O 5 10 15 20 -2 -1 O 1 2 Diameter t wrn) Distance (mm)
Figure 3.3: Size distribution of bubbles w e d in calculation and the the beam profiles of the
t~unsducers used in experiment.
the measurement, pumps were not used, instead, the flow was gravity-fed. A magnetic
stirrer was used to reduce the effects of floatation of the bubbles, but the stirrer was set to
the minimum speed. Agent exposed to ultrasound was not reused For data collection. Since
many contrast agents start to decay after preparation or dilution as a result of Koatation
and passive dissolution, all measurernents were made within 20 minutes of dilution.
Two kinds of noise data were collected. The random noise fiom the receiver and
associated electronics was collected without transmitted ultrasound. Random noise cannot
be subtracted directly kom the contrast agent signak, instead the noise power vins subtracted
from the power spectra. AU the combinations of attenuation and oscilIoscope gain settings
were tested. The signais due to electromagnetic interference £rom the transmitter and scatter
Frequency (MHz)
O 2 4 6 8 10 12 14 16 Frequency (MHz)
Figure 3.4: Pozuer spectm of simulated responses jbm the four-cycle (top) and one-cycle
(bottorn) pulses. The numbers repîesent incident peak-to-peak focal amplitude.
C . T E R 3. FXPE-NTAL VERIFTCATION 66
from solid structures (such a s the flow cell) was coilected with the transmitter t m e d on
but without contrast agent. Ekctromagnetic and acoustic interference is correlated and,
therefore, the signds from 1000 puises were averaged to e h i n a t e fandom noise. -AU the
transmitted amplitudes (70 kPa to 3.8 MPa) were tested. At each incident peak-to-peak
focal amplitude Pa, scattered echoes from 99 pulsing events were recorded and the mean
power spectnim was then calculated and corrected for the transducer frequency response and
noise. The suit able interference signal (according to transmit ted amplitude) was subtracted
from each of the 99 echoes. The Fourier power spectra were then calculated from each echoes
and then averaged. Finally the suitable noise power spectrttm (according to attenuator and
oscilloscope settings), which is itself generated from 99 traces, was subtracted from this
averaged power spectnun. The variance of the corrected power spectnim was also calaulateci
using the variance of the raw spectra and of the noise spectra.
cond harmonic
3.3 Results
The results are plotted in figure 3.5. It is de ar that se scattering near 10 MHz
is conspicuous and increases more rapidly than fundamental scattering. Spectral broadening
is also obsenred, especially around 3 and 7.5 MHz. Scattering coefficients were calculated
as the total energy detected within a fiequency band divided by the peak incident intensity.
Notice that, if a power law dependence is asnuned between second harmonic component P2/
and the incident amplitude PA, that is, P2f a c, then the scattering coefficient qf d l be
. . -
S . .
Frequency (MHz)
Figure 3.5: Power spectra of scattered signal from the four-cycle (top) and one-cycle (bottom)
pulses. Numbers represent inczdent peak-to-peak amplitude.
CHAPTER 3. EXPERlMENTAL VEmICAnON
related to Pa by
Scattering coefficients for the hindamental(0.75 fo-1 .% JO), second h m o n i c (1.75 f0-2.25 fO)
and spectral broadening (1.25 fo-1.75 fo) frequency bands for the four-cycle and one-cycle
waveforms are plotted against PA in figure 3.6 and 3.7, respectively. Simulation results are
also plotted in the same graphs, the error bars in the simulation data represent standard
error of the mean from thirty-two random subensembles.
Measured fundamental scattering was constant for PA < 500 kPa, as predicted. -4bove
0.5 MPa, the theory predicts a 3 dB depression of the fundamental scattering coefficient as
the bubbles convert absorbed energy into second and higher harmonies (Chin and Burns
2000). The measurements seem to be consistent with this prediction. For PA > 1.3 MPa,
there was a significant increase in fundamental scattering, which cannot be explained by the
present rnodel.
A quantitative discrepancy exists between simulation and measurement for the sec-
ond harmonic scattexkg. The simulation predicted that for PA < 200 kPa, second harmonic
scattering coefficient is proportional to Pfi7, whïie at higher transmit amplitudes, second
h m o n i c scattering saturates at about 8 dB below fundamental scattering. Experimental
measurements reveded an increasing power dependence. For the four-cycle pulse, the power
law coefncient below 500 kPa (the dope on the log-log plot) was approximately 0.5, and
gradudy Ïncreased to 1.2 for Pa > 1 MPa. For the one-cycle puise, the power depen-
Peak-to-peak Focal Amplitude (kPa)
i 5 f Theory 1 5 /: Ex pr.
50 100 200 500 IO00 2000 5000 Peak-to-peak Focal Amplitude (kPa)
Figure 3.6: Simvlated and measured scattering coeficients vs. incident amplitude in response
to the four-cycle pulse- (top) Fundamental (fo) and second harmonie (2 f*); (bottom) spectml
broadenzng (1.5 fo). Error bars in the simulated results indicate standard e m r using 32
ensembles.
5
0
3 - k*
8 p o c
.œ L a3 CI -1s U
V1
-20
2
Figure 3.7: Simvlated and measured scattering coeficients vs. znc2dent amplitude in response
to the one-cycle pulse. (top) Fundumental ( fo l and second harmonic (2 fo); (bottom) spectml
broadening 11.5 fo). E m r bars in the simulated results indàcate standard emor uszng 32
ensembles.
O I B I 6 6
. . . . . . .
. . . . . .
. . . . . . : . . . . . . : . . . . . . . . . E
50 100 200 500 lm 2000 5000 Peak-to-peak Focd Amplitude @Pa)
. I I r
............... . . . . . . . . . . . . . . ......:...... : : * . S . i 3%:
.II
5 Y
-20 U rA
-25
............. . . . . . . . - . . . . . . - : . :. . . . . . . . . . . . . . . .
. . ............ 1 . . . . . . . . . . . . . . . ,. . . . . . . . . . . . . . . . . - 1 S/ Theory . * 1 s t Expcr.
.
- 5 - . . - . . - . . . . . . - . . . - * . * . . . . *
.. . . . . . *S.?
. . . . . . . . . - . . . . : . . . . . . . . . . . . ErI . . . . . . . . . . . . .
2 : A ...... .:. . . . . . ; . . y . . . . . . . . . . : m.. . . . . .
r 3° - f Theory W . . . . . .:. . .d. . . . . . . . . . .:. . .A ... + PExpcr.
-30 t t * I'
50 100 200 500 Loo0 2000 5000 Peak-to-peak Focal Amplitude (Wa)
j" . & & A t * Ik * m I
- - 2, Thcory A 2 l p x p n .
dence increased from approximately 0.4 to 0.5. The occurrence of this increase coincided
with the increase in fundamental scattering. The difference between the simulation and the
experiment on the level of second harmonic scat tehg is as large as 10 dB.
Finally, as seen in figure 3.6 and 3.7 the quantitative clifference between simulation and
experiment with respect to spectral broadening is signiscant. While the simulation predicted
a very sharp increase in 1.5 fo scattering, a relatively high level of spectral broadening was
meanired ewn at PA < 500 kPa.
3.4 Discussion
Previously published studies of nonlinear scattering of contrast agents were limited in several
aspects. Most of them were conducted using continuous wave or nearly-CW bursts. Also,
a number were limited in the range of transmitted amplitude, sometimes below the lomest
output of chical scanners. In this paper, a quantitative measurement of nonlinear scattering
€rom Definity is reported. The bandwidths of the transmitted pulses were comparable to
those used in clinical irnagers. The transmitted amplitudes (MI = 0.04-1.7) ais0 cover the
range of power used in practice.
The agreement between theory and measurement was found to be generally good.
However, three specific discrepancies were identzed: (1) scattering coefficients, both funda-
mental and harmonic, increase rather than saturate for PA > 500 kPa, (2) measured second
harmonie scattering is up to 10 dB lower than theoretical prediction, (3) for the four-cycle
pulse, spectral broadening at PA < 500 kPa is signincantly underestimated by the theory.
1 Echo #I 1
1 Echo #3 1
1 - . 3
Echo #20 0.5 -
n
L 3 O
-0.5
-1 1 1 1 L
O 2 4 6 8 10 Time @s)
Figure 3.8: Optison echoes horn exposure to 2.0 MHz pulses at a pulse repetition frequency
of 2 kHz and peak-to-peak amplitude of 3.6 MPa. The first, third and twentieth echoes
demonstrate bubble shell dllsmption. The bubbles hod not been exposed to ultrasound prior
to the fi~st pulse. Sipificantly elevated fundamer-tal and hamonic scattering are obserued
aftw initial exposure, but by the twentieth echo, the bubbles have virtuaily disappeared.
The first two of these could possibly be explained by the presence of a motion-dampening
shell that is disnipted at high PA. The sheIl serves to stabilize the bubble but dampens
the motion of the bubble and reduces nonlinear scattering. There have been several reports
that contrast bubble echoes decay over millisecond timescdes under multi-pulse ultrasound
exposure (Burns et al. 1994; Dayton et al. 1999; Takeuchi 1998). The present study demon-
strates that scattering is increased during the few microseconds when the k t ultrasound
pulse strikes the bubbles. We hypothesize that this is a consequence of shell disruption. A
brief experiment demonstrates this. Pulsed ultrasound at a center Erequency of 2.0 MHz
and a peak-to-peak pressure of 3.6 MPa was transmited into a solution of Optison. Figure
3.8 shows the Brst, third and twentieth echoes from previously unexposed Optison bubbles.
The third echo, only 1 msec after the k t , produced significantly elevated fundamental and
harmonic scattering. The echoes then diminished in magnitude and effectively disappeared
within twenty pulses. It is speculated that shell dismption allows the bubbles to oscillate
more freely for the duration of a few pulses before gas dissolution reduces the bubbles to an
insignincant size. S pect r d broadening and subharmonic emission has been associat ed wi t h
cavitation events (Leighton 1997; Miller et al. 1984). Dimption of a sub-population of the
microbubbles may therefore be the source of the spectral broadening seen at low amplitudes.
3.5 Conclusions
Linear and nonünear scattering coefficients by a contrast agent were measured and cornpared
to a mode1 simulating a popdation of microbubbles. Some quantitative discrepancies were
noted, which may be explained by the presence of the bubble shell. It is suggested that
the sheU has multiple important roles in the behaviour of contrast agents. Both the basic
mechanical properties of the sheli and the effects on acoustic scattering are not yet fully
elucidat ed.
Chapter 4
Effects of Shell Disruption
Abstract l
This study is designed to investigate the effect of the shell on single-pulse scattering by a
population of contrast rnicrobubbles. Scattering was rneasured shortly (15 ps) after exposure
to a previous ultrasound pulse with variable intensity. The short time delay limits the in-
fluence of gas diffusion. The results suggest that single-pulse scattering is dependent on the
dimption properties of the bubble shell. In a previous paper, we attempted to ver* exper-
imentdy a mode1 for ultrasound scattering by a population ensemble of microbubbles. The
compsrison reveded some quantitative discrepancies between mode1 predictions and experi-
mental results. We proposed that the dimptible shell used to encapsulate the microbubbles
is responsible for the discrepancies. The results of this study c o h the significance of the
LThis chapter is based on a manascript: Chin CT and Burns PN. Investigation of the Effects of Microbubble SheU Disrtrption on Population Scattering and Implications for ModeIling Contrast Agent Behaviour. IEZE 'Ems UItrason Ferrodec Ekeq Contr (submitted).
shell properties.
4.1 Introduction
A number of factors Iimit the usefulness of mathematical theories for predicting the acoustic
response of microbubble contrast agents. Some of the difficulties relate to the multiplicity of
bubble sizes in a red population of bubbles and the heterogeneity of real incident ultrasound
fields. To account for these factors, a theoretical model for predicting the time-domain
acoustic response fkom a bubble population was created (Chapter 2). To test the model,
we measured the nonlinear scattering coefficients of the contrast agent Definity (DuPont
Phaxmaceuticals Co., Boston, MA) (Chin and Burns 1998). Gaussian-enveloped four-cycle
ultrasound pulses centred at 5.0 MHz were transmitted into diluted agent ff owing in a cell.
The scattered mgnals were detected with a broadband transducer located at 90 degrees to
the incident beam. The results generaily agreed with the model predictions, but several
discrepancies between t heoretical prediction and experimental results were apparent. First ,
measured second hazmonic scattering was up to 10 dB lower than the theoretical prediction;
second, scattering coefncients, both fundamentai and harmonie, increased rather than remain
Bat for incident acoustic pressures p > 500 kPa; hally, spectral broadening at p > 500 kPa
was significantly underestimated by the theory.
Several possible causes of the disnepancies couid be considered: themai dampening,
mass transfer and acoustic disniption. Thermal dampening is known to reduce bubble os-
cillation amplitude and therefore nonlinearitgr, however, as the incident amplitude and the
radial amplitude of the bubble increases, the effect of thermal dampening is &O increased
(Prosperetti 1991). Therefore, thermal dampening would not be expected to cause an in-
crease in fundamental and harmonic scattering at high incident amplitudes. Secondly, mass
transfer could occur by rectified cifision, a relatively well-understood process. Since the
difision rate is different during the expanded phase (when gas evaporates into the bubble)
compared to the contracted phase (when gas dissolves into the liquid), gas fiows preferren-
tially into the bubble owr a complete cycle of bubble oscillation (Leighton 1997). However,
rectified diffusion is generally believed to be a slow process that involves at least hundreds of
microseconds (Church 1989). Therefore, we focus on acoustic disruption as a possible source
of the observed behaviour.
Two factors are believed to be important in bubble disniption, the gas behaviour and
shell behaviour. When the shell of a bubble is disrupted, it is believed that its ability to
Mpede gas dissolution is compromised. The content of the bubble is allowed to dissolve into
the surroundhg liquid at an increased rate. The dissolution rate is limited by the diffusivity
constant and the solubility of the gas molecules (although some remnants of the shell may
reduce the actual dissolution rate below the free bubble level). Consequently, the lifetime of
the contrast bubbles after initial disruption is mainly determined by the gas type.
We performed two experiments, the £irst to meanue the effect of the gas type, the
second the effect of the shell. In the fkst experiment, the decay of the scattering power
was measured for an agent containhg nitrogen and an o t h e h identical agent containhg
peduoropropane. In the second experiment, the effect of a previous exposure to ultrasound
was rneasured by insonation with two pulses separated by a very short penod of time. To
isolate the effects due to gas type, the measurements were made before dissolution of the gas
could cause a measurable effect on scattering.
4.2 Method
The experimental setup is outlined in figure 4.1. A Sony/Tektronix AWG2020 (Beaverton,
OR) arbitrary waveform generator produced Gaussian enveloped pulses which were then
amplified by an ENI 240L 50 dB power amplifier (Rochester, M). Separate transmit and
receive transducers were used to eliminate the needs for nonhear circuit components. The
transmit and receive beams cross at right angle at the centre of a flow ce11 which has mylar
membranes as acoustic windows. The distance between the transmitting transducer and the
sample volume was kept short to reduce propagation nonlinearity. The scattered ultrasound
was detected by a receiving transducer at 90'. The signal was attenuated with a variable
attenuator by up to 12 dB and then amplified with a custom designed switched mgnd
amplifier. This amplifier can be switched electronicaily between gains of 35 and 53 dB.
The amplifier has a dynarnic range of 65 dB and at most -54 dB of harmonic nonlinearity.
The arnplined signal was then Giltered with a custorn 1-16.5 MHz bandpass filter to remove
noise and digitized at 50 MHz with 12-bits resolution with a Gage PDA 8012A (Montreai,
Canada) A/D converter installed in a personal cornputer. This setup effectively ehinated
interference from direct acoustic couphg or solid structure reflection, dowing measurements
at transmit pressures below 40 kPa.
In the first experiment, the agents were exposed to dtraçound pulses at a pulse
CHAPTER 4, EFFECTS OF SEIELL DISRUPï7ON
54/34 dB
Figure 4.1: Ezperimental setup for the nonlinear scattering rneasurement.
repetition frequency (PRF) of 2 kHz. A pair of Picker (Highland Heights, OH) 3.5 MHz
transducers were used as the transmitter and receiver. The ultrasonic pulse used had a
centre fiequency of 2.2 MHz and the Ml-width-half-maximum pulse length was equal to
2.9 periods. The diluted agents were allowed to flow for 20 seconds in order to cornpletely
refiesh the bubbles. The flow was then stopped and the suspension allowed to settle for
30 seconds before ultrasound pulses were transmitted. The echo data were collected for
2 seconds, and the process was repeated ten tirnes. The agents tested were Definity and
a special experimental formulation of Defini@ in which the perfiuoropropane was replaced
with nitrogen.
The second experiment focussed on the effects of the shell. Inference of the significance
of shell was made fiom measurements on several different agents. These agents cover a range
of gas types and sheU properties. Four contrast agents were available for this study: Levovist,
Sonavist (Schering Ag, Berlin), Definiw (DuPont Pharmaceuticals Co., Boston, MA) and
Optison (Mnllinckrodt Inc., St. Louis, MI). Table 4.1 lists their constitution and properties.
Table 4.1: The constitution and pmperties of the contrast agents used in the shell effect experinrent.
..
The agents, flowing continuously, were exposed to two ultrasound pulses (5.0 MHz,
FWHM = 3.7 periods) separated by 15 p. The first pulse had variable amplitude (p,) and
the second pulse had a h e d arnpütude (pb) , as shown in figure 4.2. The first pulse rneasured
the amplitude dependence of the acoustic response of the bubbles. The second pulse detected
any changes to the scattering properties caused by the exposure to the first pulse. A Matec
(Northborough, MA) 5.0 MHz transducer (aperture f/2, focal length = 19 mm) was used
as the transmitter and a Blatek (College Park, PA) 6.5 MHz transducer (aperture f/4, focal
length = 38 mm) was used as the detector. The switched amplifier was designed to allow
both the first and second echoes, which had power clifference of up to 24 dB, to be digitized
with hi& fidelity. The pulse pairs were repeated at a PRF of 40 Hz. Flow velocity through
the sampled volume was rneasured independently to c o b suf6cient refreshment of the
bubbles between pulse pairs. The diluted contrast suspension was ftowed through the celI at
a d ic ien t ly fast rate that the sensitive volume of the transducers was refieshed with bubble
as each pulse pair amves, while the delay was short enough to effectively freeze the bubble
displacement.
For each agent and for each first pulse amplitude (p,), two hundred echo pairs were
Levovist Sonavist Defini@ O~t ison 1.
Gas type air air
C3Fs
Shell solubiüty/diffusivity
high high iow
me palmitic acid
p o l p e r p hospholipid
,, CIIFSH~
cornpliance high low high
. low 11 albumin . medium
First Pulse Second Pulse 40-2000 kPa 240 kPa
Figure 4.2: The pulszng sequence used in the shell e h t s meusurement.
recorded. Ail measurements were performed in l e s than 30 minutes after preparation or
dilution, this ensured that the agent properties had not changed significantly by passive
processes. Data were dso collected without scatterers in the Bow ce11 so that extraneous
power due to noise and interference could be subtracted during analysis. The recorded
data were andyzed o f i e using Matlab (The MathWorks Inc, Natick, MA). The power
spectra were calcdated, and the noise power spectra were subtracted. The spectra were then
corrected for the receiver fiequency response, and the power spectrum due to interference
is subtracted as the last step. The fundamental (fo), second h m o n i c ( 2 f o ) and spectral
broadening (1.5 fo) scattering coefficients were measured fkom these spectra using a width of
0.5 fo eaeh.
From the fmt experiment, each rneasurement consisted of 4000 consecutive echoes from the
stationary agent. For each agent and at each incident amplitude, typically ten to twelve
(minimum seven) independent measurements were made. An =ample of five of the k t
forty-one echoes are plotted for one measurernent at 1.8 MPa (peak-to-peak) for each agent
in figure 4.3. The special Definity (Nz) was a weaker agent, therefore, the echoes for the
regular Definity (PFC) were scded by a factor for display. Noise power was subtracted from
the echo power. The time it took EtbfS echo amplitudes to drop to half the maximum level
was measured a s the Iifetime. The means of these lifetimes were plotted against incident
peak-to-peak amplitude in figure 4.4.
For the second experiment, fundamentai (fo), second h m o n i c (2 fO) and spectral
broadening (1.5 fO) scattering were measured from both echoes. An example of three echo
pairs for Sonavist are plotted in figure 4.5. The first two of these pairs, having been exposed
to amplitudes of 262 kPa or lower, showed good correlation between the first and second
echoes of the pair and dernonstrated comparable scattering coefficients. In the 1 s t pair, with
an exposure of 3034 kPa, scattering fkom both the first and second echoes were elevated.
These meanirernents fields on (p,,pFe) which are the scattering coefficients at nth harmonic
(n fo) as b c t i o n s of incident pressure amplitude p, and amplitude of previous (if nonzero)
puise p,,. Thus, the first echo yielded q (p,, O), 02 (pw , O) and ais (p,, O) and the second
echo yidded ol (pb, pu), 02 (pb, pw) and 01-5 (pb, p,) where pw was varied from 33 kPa to 3034
kPa and ph was held constant a t 260 kPa. The results are plotted in figures 4.6 and 4.7.
C ' T E R 4. EFFECTS OF SHELL DISRUpcITON
PFC (v / 4.46)
Figure 4.3: The Ist, Ilth, 21st, 31st and 41st echoes from one of the measured data set for the regular Definity (PFC) and the specàal Definity (IVz). Each trace was 10 ps in length. PRF = 2 Mit, pp = 1.8 MPa. The PFC echoes (voltage) were scaled by a factor of 4.46 since the special N2 DefiBity tuas a weaker agent.
4.4 Discussion
Several authors have reported on aspects of acoustic disruption. Uhlendorf and Hoffmann
(1994) mesnired nonlinear scattering fiom the agent Sonavist usine; long (35 cycles) bursts
of 5 MHz ultrasound. It was suggested that the transient nonlinear response, called "Acous-
tically Stimulated Acoustic Emissionn , is a result of the mpture of the bubble shell. Morgan
et al. (1998) showed opticdy that a single ultrasound pulse can be sufncient to initiate the
cornplete dissolution of contrast bubbles. Chomas et al. (1998) made optical and acoustic
measurement on microbubbles under medium to high ampiitude (0.8-2.6 MPa) ultrasound
for an experimentd agent with a Lipid shell and high rnolecular weight gas core. Dayton
O 1 2 3 4 5 Incident Amplitude (MPa)
Figure 4.4: Lifetimes (defined os tzme for the RMS amplitude of the echoes to drop to half the mmimum level) us. incident amplitude for tmo agents &th different gas types.
et al. (1999) made detailed optical measurement on two agents with different shell materials
and noted that the difference in acoustic response to a train of ultrasound pulses might be
related to the differences in shell materials. Frinking et al. (1999) demonstrated that the
agent Quantison can release fiee gas bubbles after exposure to a high amplitude burst (1.6
MPa, 10-cycle at 0.5 or 1.0 MHz). When probed 0.6 ms after the high amplitude burst, the
fiee gas bubbles produced 15-20 dB more fundamental scattering and 10 dB more relative
harmonic scatt ering compared to intact Quantison part icies.
In this study, two experiments were performed to iderit* the effects of dtrasound ex-
posure to contrast agents- In the fkst experiment, the agents are exposed to multiple pulses
transmitted at a PRE' of 2 kHz. As the incident amplitude increased, the echo decay time
CiNtlPTER 4. EFFECTS OF SHE:LL DISRUPTION
First Echo Second Echo
Figure 4.5: Pairs of echoes frorn Sonavist fiom diferent first pulse amplitudes ( p J . The delay between the Jirst and second echoes is 15 ps. Each trace was 5 ps in length and uas nomalited Qy the correspondzng (frst or second) incident amplitudes. Notice that at the hzghest p,,,, 60th the fist and second echoes were elevated.
decreased from about 1000 msec to a minimum of 2.6 msec. The special Definity contain-
ing nitrogen disappears about two to ten tirnes faster than the regular Definity containhg
peduoropropane. This established that gas type has a strong effect on the decay of bubble
echoes and that gas dissolution over the microsecond timescale is negligible.
The second experiment was designed to detect changes on the microsecond timescde
caused by a single dtrasound pulse. From figure 4.6, Definity (DMP-1 E), Optison (FSO69)
and Levovist (SHU508a) aU demonstrated fundamental scattering remained essentially con-
stant, with a s m d (about 2 dB) decrease at high amplitudes (p, > 500 kPa), in agreement
Figure 4.6: F W pvkre scattering coefieients for the four contrast agents
?
Second Pulse fo So08vist f Opison '
Ddinity trvov Mt
1
Frrst Puise lecidtnt AniDliaxdt &Fa)
Figure 4.7: Second p d e smttMg coefiieents for the four eontsast agents
with the theory Nonlinear scattering (a2 and ois) for a.il agents increased with increasing p,.
Figure 4.7 shows that the second pulse scattering of both Dennity and Optison was relatively
unaEected by the amplitude of the first pulse. Finaily, Sonavist (SHU563a) demonstrated
drûmatic increases of both linear and nonlinear scattering for incident amplitudes above 500
kPa. Figure 4.7 shows the dependence of h e m and nonünear scattering on ultrasound ex-
posure history. Sonavist demonstrated significant increases in the second pulse scattering;
in particular 01.5 was boosted by more than two orders of magnitude.
hpart fiom the dependence on the incident amplitude p,, acoustic scattering is
demonstrated to be dependent on contrast agent and disruption by strong ultrasound pulses.
First pulse nonlinear scattering is the lowest in undisrupted Sonavist, ranging Erom unde-
tectable to about 50 dB below fundamental scattering level; it is intermediate in Levovist,
Optison and Definity, ranging &om 60 to 20 dB below fundamental scattering level; and
the highest in disrupted Sonavist, ranging from 50 to 8 dB below fundamental scattering
level. Increases in scattering coefficients from the second echo were observed from Sonavist
at incident amplitudes higher than 400 kPa. This corresponds to the ciramatic increases in
first pulse scattering and is consistent with a steep threshold of disruption of the agent's stiff
po1per shell. Spectral broadening (oId) was consistently detected in agents with a flexible
shell. In Sonavist, spectral broadening is detected only during and after acoustic disruption.
The results support the hypotheses that (1) nonlinear (2fo and 1.5 fo) scattering is
related to sheU flexibility; (2) increased single-pulse scattering at hi& incident amplitudes
is associated with acoustic disntption of the bubble shelI; and (3) spectral broadening is
asociated with shelI disniption and is observed at low incident amplitudes fiom agents with
CHAPTER 4. EFFECTS OF SHELL DISRUPTION
a flexible shell.
4.5 Conclusions
Previously, ultrasound contrast agents were broadly classified as either diffusible (air-based)
or non-difhisible (PFGbased) agents. Diffusible agents decay quiddy when evposed to a
series of ultrasound pulses over millisecond timescales, and non-dfisible agents can sur-
vive upto thousands of milliseconds. By isolating the effects of shell type lrom gas type,
the present work demonstrates that shell properties have a strong iduence in the acoustic
response of contrast microbubbles over microsecond timescales, indicating that the shell, as
well as the gas, is an important determinant of bubble behaviour in an acoustic field.
Chapter 5
Applications and Future Prospects
5.1 Introduction
During the course of my research, some developrnents of contrast irnaging methods changed
our perspective on the importance of stable hannonic scattering by microbubbles. Section
5.2.1 describes the development of intermittent imaging, which provides superior sensitivity
at the expense of imaging frarne rate since the bubbles are disrupted by the imaging pulses.
Intermittent imaging produced the first perfusion images of the myocardium, which was
considered the HoIy Graii during the introduction of encapsulated agents. For a period
of t h e , imaging methods that were sufnciently sensitive were d l disruptive, and it mas
thought that the role of a nondisiuptive bubble scattering mode1 wodd be diminished. More
recently, highiy sensitive nonlinear imaging met hods were developed. These met hods, w hich
are reviewed in sections 5.2.2 and 5.2.3, have d c i e n t sensitivity to image blood Bow in the
myocardium and other demanding situations using low h1I puises which are non-destructive
CHAPTER 5. APPLICATIONS AND FUTURE PROSPECTS 91
or mildly-destructive. As a result of these developments, the interest in a nondismptive
model is revived. A number of questions relating to the basic mechanisms of these rnethods
remain unanswered. The bubble model presented in Chapter 2 was used to investigate some
of these questions in section 5.3.
h o t h e r area of future development is the application of contrast microbubbles in
high fiequency ultrasound. Section 5.4 presents preliminary theoretical and experimental
results of noniinear scattering by a contrast agent.
5.2 Recent Developments in Contrast Imaging
5.2.1 Intermittent Imaging
The combination of harmonic filtering (which detects the second harmonic scattering) and
Doppler mode (which detects motion of the scatteren) was demonstrated to be sufficient
to detect blood flow in vessels as small as 44 pm in a kidney (Burns et ai. 1994), which is
relatively stationary and well pemised. However, irnaging of myocardial blood Bow presents
a greater challenge. The v a s d a r space accounts for ordy 10-15% of the volume of the
myocardium, limiting the number of microbubbles that contribute signal intensity. The
motion of the myocardium itself is much greater than the motion of the blood relative to
the tissue, rendering the Doppler technique useless in blood fiow detection. A significant
advancement was made possible by Uhlendorf and Hoffmann (1994) when they reported
disruption of microbubble echoes within a few milliseconcis. The fast decay or decorrelation of
the contrast echoes appears indistingnishable fkom that fiom scatterers moving very quickiy
(XU..PTER 5. APPLEA'MONS AN. FUTURE PROSPECTS 92
through the imaged volume. As a result, pseudo-Doppler signals can be detected. Such an
observation led to the development of a highly sensitive contrast imaging strategy enploying
strong (MI > 1.0) dtrasound and hannonic Doppler detection. Since the method relies
on the dismption of the contrast echoes, continuous redtime imaging is not possible. .!fier
each frame of image is obtauied, transmission of ultrasound must be suspended to allow Eresh
microbubbles to enter the imaged volume. In the myocardium, N1 recovery of the contrast
signals in the hedthy myocardium takes 4 to 8 seconds (Linka et al. 1998). As a result,
€rame rates as low as 0.1 Hz are used. Such a technique was called intermittent imaging
or interval-delay imaging. Imaging of myocardial blood flow was reported by Porter et al.
(1995, 1996). In the liver, the evolution of signal intensity frorn intenml-delay irnaging was
correlated to vascular volume and was demonstrated to improve characterization of lesions
(Wilson et d. 2000).
5.2.2 Pulse Inversion Detection
There is a tradeoff between axial resolution and achievable contrast in harmonic imaging (see
section 1.4.2). This is because axial resolution is fundamentdy related to the bandwidth
of the transmitted pulse. A fher resolution requires the use of a wider bandwidth which is
detrimental to discrimination between the fundamental and hannonic echoes based on the
frequency (figure 5.1). Pulse inversion detection (PD) (Hope Simpson et al. 1999) was
invented to address this problem.
Pulse inversion exploits the fact that nonlinear scattering violates the hearity prin-
C W T . 5. APPLICATlOn'S AND FUTURE PROSPECTS
Figure 5.1: When a high axial resolution is desired, generolly a wide bandvidth is used.
However, the abilzty of homonie imaging to discriminate between findamental and harmonic
f+equencies is h i t e d by ouerlapping banduidth.
ciple, equation (1.22). Specificdy,
Therefore, the pulse inversion strategy c d h for two pulses with opposite signs (pin and -pin)
to be transmitted instead of one. When each pair of echoes (pcchol and pedio2) are collected,
they are summed together h t o a single echo signal and images were constmcted using the
sum signds. For Iinear scatterers, the sum signal is zero. For nonlinear scatterers such as
microbubble contrast agents, the sum signal is nonzero (figure 5.2).
A conceptual tool used by severd authors (Hope Simpson et al. 1999; Jiang et al.
1938) eonsists of a simplified model for the harmonic scattering by microbubbles. In this
model, harmonies are produced by assuming that the scattered pressure follows a polynomial
CHAPTER 5. APPLICATIONS AND FUTURE PROSPECTS
Figure 5.2: Pulse Inversion Deteetion. A pair of incident pulses &th opposzte signs are
h 10
cJ a M *a
P- -IO
tmnsmitted. The echoes are summed together, the fvndurnental component is cancelled out
Pa,, + P&2
oJIb 1
li*
7
und the even hamonic components are preserved. The echoes were calculated for a 1.9 prn
diametw fkee bub ble. Incident peak-to-peak amplitudes were 300 kPa and 150 kPa.
O 1 2 3 Time (CLS)
CEfWPTER 5. APPLICATTONS AND FUTURE PROSPECTS
relation to the instantaneous pressure of the incident wave:
where al, al etc. are constants. The rationale for equation (5.2) is that, for continuous wave
excitation,
Pin = p-4 COS (ut) ,
then each even power term P;! will produce even harmonies of orders 0,2,4, ,272; and
*"+' Will produce odd hmonics of orders 1,3,5, - , Zn + 1: each odd power term pin
4 a4 + 7 + p, - + *) cos ( 2 4 + p q + - .) cos ( h t ) 2 ( 3 a 3
+ + .) cos (4'dt) +
If only al and a* are nonzero, then equation (5.4) predicts that second harmonic amplitude
to be proportional to the second power of the incident pressure amplitude, the same as
predicted by the weakly nonlinear approximation used by Milier (1981).
While a visual inspection of any scattered waveforms, such a s the second row of figure
5.2 would suggest that the polynomial mode1 is very iimited in accuracy, it has proven to be
useful in the early conceptual development of multi-pulse non-destmctive detection methods,
CHAPTER 5- APPLTCAïTONS AND FUTURE PROSPECTS
such as pulse inversion. Applying equation (5.4) to PD, one obtahs
so that the linear scattering term, p ~ a l cos(2wt), dong with ali the odd harmonic terms,
me cancelled out and aU the even harmonic tems are preserved. Therefore, by using two
pulses, PID d o w s discrimination of the linear component of the echo without the use of a
filter which limits axial resolution. The method was extended to allow more than two pulses
to be used, thus adding motion discrimination to two-puise pulse inversion.
Recently, multi-pulse PID has achieved sufficient sensitivity so that constrast bubbles
can be detected without using high transmitted pressures which destroy the bubbles. Sub-
sequently, redtime imaging of myocardial blood fiow in human patients was demonstrated
(Tiemann et al. 1999). The ability to image at a frame rate of 15 Hz or higher is a major
improvement over intermittent imaging.
5.2.3 Power Modulation Imaging
Another method closely related to pulse inversion is based on the Following violation of the
hearity equation:
Power modulation irnaging (PMI) operates by transmitting two pulses of different amplitudes
(pin and pin/2) and then u h g a weighted difference - 2pcend) of the two echoes to
(3UPTER 5. MPLlCATPfONS tU\JD FUTURE PROSPECTS 97
cancel the linear signal (Jiang et al. 1998). Figure 5.3 illustrates the operation of PMI using
the same bubble as figure 5.2.
Using the polynomial mode1 again, the resultant signal is given by
- + *) cos ( 3 4 + + - cos ( k t ) + - - . (5.7) + ( P i 2 '" 64 1
While the Linear scattering tem, p ~ a l cos(2wt), is cancelled out, nonlinear t e m s of both
odd and even orders are preserved.
Considering only the linear and quadradic t e m s (al and a*) and using a signal-
t+noise ratio approach, Jiang et al. (1998) argued that PID should be superior to PMI.
Since then, however, both methods have been implemented on commercial scanners and
clhicai experience has shown both methods to be cornpetitive as realtime rnodalities for
rnyocardial perfusion imaging. The explanation of power modulation's success starts with the
recognition that a3 # O and a non1inea.r scattering component is preserved at the fundamental
frequency: s p i a 3 COS (ut), see equation (5.7). Therefore, PMI was configured to operate at
the centre of the transducer bandwidth (Brock-Fisher et al. 2000). By foregoing the second
hannonic echoes, both the transmitted waveform and the received echoes are placed within
the same frequency band. This has the important advantage that the fidi bandwidth of the
transducer is used for both the transmission and reception processes. In contrast, PID must
be configured so that the centre frequency of the transmitted waveform is placed somewhere
in the lower half of the transducer bandwidth, resulting in the second harmonic echoes
CHAPTER 5. APPrTCATPT"NS AND FUTURE PROSPECTS
- -
O 1 2 3 Time (CLs)
Figure 5.3: Pover Modulation Imaging. A pair of incident pulses urith different amplitudes
are tmnsmitted. A weighted diference of the echoes is used to cancel the linear component.
AI1 honnonic components are p~eserued- The echoes were colculated for a 1.9 prn diameter
j k e bubble. Incident peak-to-peak amplitude was 300 kh.
C W T E R 5. APPLICATlONS AND FUTURE PROSPECTS 99
appearing within the upper half of the transducer bandwidth (figure 5.4). However, the
better exploitation of the transducer bandwidth may corne at the cost of reduced bubbles
response. It c m be expected the third order nonlineazity which gives rise to the detected
signal in the PMI scheme is lower than the second harmonic component which is detected
by PD. However, the relative merits of the two methods are currently unknown, since the
polynomial bubble mode1 (equation 5.2) is not supported quantitatively by any theoretical
or experimental evidence.
5.3 Applications of the Bubble Mode1
.4t present, the relative strength and weakness of pulse inversion imaging and power modula-
tion imaging are not f d y understood. .4s Far as a clinician is concemed, these two methods
must be compared as fuUy implemented imaging modes on cornmencal scanners in a clinical
setting. However, actud implementation on a machine involves many factors that make it
dificuit to identify the factors that determine the performance of each method. Further-
more, commercial and Iegal concerns often ümit opportunities to test experimentaily these
methods in a comparable rnanner. One key question is: given that contrast agents Molate
ünearity in both the sense of ttsign" (equation 5.1) and the sense of "proportionality" (equa-
tion 5.6), which type of nonlinearity is stronger? When this question is ansnrered, the other
effects, such as nonlinear propagation, kequency-dependent attenuation, frequency response
of the transducer, electronic noise, etc, can be added so that each method can be rigourously
optîmized and compared.
CHAPTER 5. APPLICATIONS AND FUTURE PROSPECTS
O 1 2 3 4 5 6 Frequency (MKz)
O 1 2 3 4 5 6 Frequency (MHz)
Figure 5.4: Pukre Inversion Detection (PID) and Power Modulation Imaging (PMI) employ
the limited bandwidth of the transducer differently. The dashed line represent the fiepency
response of a hypothetical transducer with 100% bandwidth. PID bene@ from a higher
nonlinear response, while PMI benefits from the full exploitation of the transducer bandwidth.
The purpose here îs to demonstrate the application of the scattering model in the
optimizatîon of low-intensity nonlinear imaging methods. It is instructive to consider an
individual bubble of the resonant size. In this discussion, several factors are not included.
Where a quantitive analysis is desired, a number of factors can be readily added: the distri-
bution of bubble sizes, attennation and nonIinear propagation in the tissue, and, especidy,
beam dïfbaction pattern. Figure 5.5 shows the scattered waveforms of a 1.9 Fm bubble
CHAPTER 5. APPLICATIONS IWD FUTURE PROSPECTS 101
in response to a 5 MHz ultrasound puIse with positive phase. As the incident pressure is
increased, the scattered waveforms become distorted, producing harrnonic components (see
also figure 2.3). Figure 5.6 shows the corresponding results using the PID and PMI schemes.
Figure 5.5: Scattered waveforms of a 1.9 pm bubble in response to a 5 MHz incident pulse
(FWHM pulse duration = 1.2 cycles). Euch wavefonn is nomalzzed by the incident pressure.
Sizteen different incident pmssures (peak-to-peak) spannàng 1 to 1000 kPa were simulated.
Figure 5.6 shows that, like harmonic irnaging, both Pm and PMI produce increasing
response with respect to incident pressure. The frequency spectra of some of these waveforms
are plotted in figure 5.7. Once again, as incident amplitude is increased, second and third
harmonic cornponents appear, and ha l ly the bubble produces spectrally broadened signais,
which is the result of the unevedy spaced sharp pressure pesks seen in the Iast few c w e s of
CHAPTER 5. APDDICATTONS AlVD FUTURE PROSPECTS
Figure 5.6: Result of PID (top) and PMI (bottom). The Y-& values comspond to the
amplitude of the first (stronger) pulse. Each wauefonn is normatized by the incident pressure.
CHAPTER 5. APPLKAïTONS AND FUTURE PROSPECTS 103
figure 5.5. P D (middle panel), as expected, preserves the second harmonic component while
surpressing the linear signal at fo. However, a s m d amount of fundamental scattering (about
-18 dB fiom the 2 fo component) is observed for 10 kPa and 100 kPa incident amplitudes. This
is the resutt o fa nonlinear component of the fundamental scattering that is dependent on the
phase of the incident pulse. This nonlinear component is not predicted by the polynomical
model. PMI (bottom panel) demonstrates a lower performance at both fo and 2f0 at the
lowest amplitudes (10 kPa or less). At 100 kPa, a significant amount of scattering at JO
appears, which corresponds to the "third order nonlinearity" predicted by the polynomial
model.
An amplitude of 100 kPa corresponds to M l = 0.045, which is a relevant amplitude
for realtime perfusion imaging. At thîs amplitude, PID produces significant amount of
2 f0 signds and PMI produces dmost equal amounts of fo and 2fo signals. However, an
inspection of figure 5.7 reveals that quantitative merits of these methods will also depend
on the bandwidth of the transducer. In an attempt at a ''fair" cornparison, diEerent centre
frequencies transducers have been assumed for each methods (figure 5.8). For PID, a centre
frequency of 1.5 fo was used, and for PMI, a centre fiequency of fo was used, in both cases, a
fractional bandwidth of 50% was used. Using these assumed transducer fiequency responses,
the performance of P D and PMI can be quantitatively compared in figure 5.9. For incident
amplitudes below 300 kPa, PID outperforms PMI, however, 300 kPa ( M I = 0.13) is still a
useM amplitude for redtime perfusion imaging. Thedore, the bubble scattering model is
able to explain the comparable performance between P D and PMI.
CKAPTER 5. APPLICA2TONS AND FUTURE PROSPECTS
- 1 Power Modulation 1
"- O 0.5 1 1.5 2 2.5 3 3.5 4
Frequency I fo
Figure 5.7: &quency spedra of single pulse echoes (top), and the results of the PID (mid-
dle) and PMI (bottom) methoh. The numbers next to the m e s indzcate the peak-to-peak
incident amplitudes.
CHAPTER 5. APPLICATTONS AND FUTURE PROSPECTS
Transmitted amplitude (kPa)
Figure 5.8: Assumed jkquency response of the transducers for the cornparison of PID vs.
PMI methods.
Figure 5.9: Relative performance of PID and PMI using the frequency responses in figure
C W T E R 5. MPUCATIONS AND FUTURE PROSPECTS
5.4 Nonlinear Scattering at High Frequency
High freqency (2û-200 MHz) ultrasound h a . been applied to detect (Christopher et al. 1997)
and map (Goertz et al. 2000) blood Bow in individual vessels as small as 10 Pm. Contrast
agents c m potentialiy improve the sensitivity of these methods by enhancing the blood flow
signal relative to the surrounding tissue and noise. Using equation (1.14) and figure 1.3,
one can predict the size of bubbles that resonate at these high frequencies, for example, the
resonant diameter a t 20 MHz is 0.65 Pm. FVhile bubbles smaller than 1.0 prn can not be
sized accurately, their presence can be optically obsewed. Therefore: theoretical simulations
and acoustic experiments were performed at this frequency.
For the sake of sirnplicity, a consideration of single bubble response to 2.0 MHz and
20 MHz ultrasound pulses are compared. Generally scattering cross-section decreases a p
proximately with the bubble size, therefore it is expected that scattering foc high frequency
is weaker. However, the number density of mall bubbles is expected to be higher. Since
quantitative size distribution below 1.0 pm is not available, only an order of magnitude can
be roughly estimated by extrapolation. The size distribution of Definity follows an exponen-
tial relation from 1.0 to 15 Pm. Extrapolating this relation down to 0.65 Pm, one obtains
a number density ratio of 6.3 between 0.65 pm and 4.0 pm (the resonant size for 2.0 MHz)
bubbles. Even with the advantage of higher bubble density, the s m d bubbles are stiU Iess
efficient a t h e a r and nonlinear scattering than the 4.0 pm bubbles. However, when higher
incident amplitudes are used, comparable responses can be obtained fiom the higher fre-
quency. Figure 5.10 shows that echo responses with comparable harmonic components can
CHAPTER 5. APPL.ICA?TTnhfS AND FUTURE PROSPECTS
50 20MHz 200kPa 2 MHz 50 kPa
8 40 w
3 330 3
8 < 20
10
O
Figure 5.10: Simuloted bubble echo spectm for: 0.65 pm bubbles in 20 MHz ultrasound
pulses at 200 kPa (black) and 4.0 pm bubbles in 2 MHz ultmsound pulses ut 50 kPa (red).
The echo power/rom We smaller bubbles was increased by a factor of 6.3 to account for the
higher number density.
be obtained, albeit different acoustic conditions are required.
Nonlinear scattering at 20 MHz was measured from Definity (Dupont Phaxmaceuticals
Co., Boston, MA) in collaboration with Sarah Wong and David Goertz. A scaied-down
version of the expenmental setup shown in figure 3.1 was used. The transmitting and
receiving transducers were custom made for high resoIution mouse imaging in Dr. Stuart
Foster's laboratory. The transmitter has a peak freqency response a t 19 MHz and the receiver
has a peak frequency response at 40 MHz; both transducers have fractional bandwidths of
about 100%. Since s i p a l to noise ratio was a s i g n i b t limitation at these frequencies, the
bandwidth of the transmitted pulses wsç set be to narrower than the pulses used in Chapters
CHAPTER 5. APPLICATTONS AND FUTURE PROSPECTS 108
2,3 and 4; the fd-width-haif-maximum pulse lengt h was 5 periods (at 20 MHz). Figure 5.11
shows the averaged echo spectra fkom Definity and suspended graphite powder. The plotted
power spectra were corrected for the frequency responses of the receiving transducer and
electronics. The transmitted pressure was approlcimately 2.6 MPa, which was significantly
higher than the amplitude used in the calculation (figure 5.10). At this high amplitude,
nonlinear propagation produces a significmt arnount of harmonics, as demonstrated by the
result fkom graphite powder. Nonetheless, the nonlineax scattering is dernonstrated by a
second harmonic component that is 8.5 dB higher than the graphite powder. Even more
conspicuously, significant amount of spectral broadening was detected around 0.5, 1.5 ad 2.5
O 10 20 30 40 50 60 70 Frequency (MHz)
Figure 5.11: Averaged power spectm of 1000 echoes for Definity (solid) and gmphzte powder
(dashed). The result from graphite powder demonstrate second and thzrd harmonics (40
and 60 MHz) due to nonlineur propagation; the additional sipals at these peuh, as vell as
spectral bmodening, are due to the nonlinear scattering by the contrust bubbles.
C W m 5. APPEA'MONS ANCI FUTURE PROSPECTS 109
fo. These signds are likely associated with agent destruction as the incident amplitude was
very high. This result represents one of the fht harmoaic measurements hom ultrasound
contrast agents at such a high incident fiequency. W e the low signal-to-noise ratio is stül
a iimiting factor for imaging applications, the possibility of detecting nonlinear scattering
from contrast bubble does open the oppotunity for applications at a very fine scale.
Chapter 6
Conclusions
In this thesis, efforts to develop a purely mechanistic model for the prediction of nonlinear
scattering by microbubble contrast agents were presented. A number of models for the radial
motion of a single bubble were reviewed. A model was developed from Trilling's equation
with a number of minor modifications for applications to ultrasound contrast agents. This
single bubble model was extended to a population model employing a multiplicity of bubbles
with a realistic size distribution placed in a realistic heterogenous sound field. The inclusion
of a range of bubble diameters d o m the model to respond to a broad range of fiequency,
unlike the single bubble model. The heterogeneity of the sound field addresses the limitation
of using MI, which reflects the pressure amplitude ofonly one point in the field, for nonlinear
imaging applications.
A quantitative test of the model's prediction of nonlinear scattering was carried out.
The experiment was one of the first quantitative measurements of the h e a r (JO) and non-
h e a r (2 fo and 1.5 fo) scattering by a contrast agent to diagnostic ultrasound pulses. Exper-
imental data were collected from previously unexposed bubbles in order to avoid disruption
effects by strong incident ultasound pulses. The results confirm the generd validity of the
model, but some quantitative discrepancies were observed.
Consideration of these discrepancies and the limitations of the rnodel led to the hy-
pothesis that shell effects may play an important role in single pulse scattering. A second
ultrasound pulse was used to probe the hypothesized effects due to sheil disruption. Effects
due to the gas dissolution were isolated by using a very short time delay in the two pulse
experiment. The results demonstrated the significance of shell disruption in single pulse
scat tering.
6.2 Limitations
Severd factors still limit the potentid of the microbubble population scat tering model. Some
of these are the same ones that limit the clinical applications of other ultrasound techniques
such as tissue characterization. These generdy involve lack of accurate knowedge of attenu-
ation and aberration of the incident ultrasound beam by tissue layers. The most important
consequence of this is the uncertainty of the in vivo incident ultrasound amplitude. Another
problem is the lack of knowledge of sheU properties and bubble size distribution in vivo.
A more accurate description of acoustic disruption, bot h by t heoretical and experimental
means, is also greatly needed. These problems are actively being addressed by many workers
CHAPTER 6. CONCLUSIONS 112
in the field. One can envision that, with some answers that wiU no doubt appear in the near
future, the present theory can be extended to form a complete description of ultrasound
contrast imaging.
While the current model cannot account for the shell disruption effect, the value of
the model is in fact demonstrated by the identification and measurernent of the shell effects.
By making quantitative predictions based on known or hypothesized rnechanisms, one of the
most important values of a model is to draw attention to experimental observations that
are unexpected or incompatible with the hypothesized mechanisms. It is beüeved that the
population scattering model, which in the hture may include modifications to account for
disruption and other effects, will continue to contribute new interesting questions in the field
of contrast imaging.
6.3 Future Directions
6.3.1 Single Bubble Mode1
In chapter 4, it was established that a dimptible shell is the most important cornponent
currently missing hom the single bubble model. A nurnber of approaches have been used
in attempting to account for the shelI. The simplest approach assumes that the shell is
made of a homogeneous elastic solid that obeys Hooke's law. Assuming the radial motion to
be small (in the linear regime), the shift to the resonant frequency (see equation 1.13) was
obtained (de Jong et ai. 1992). de Jong also introduced a shelI friction factor analogous to
the viscous loss. By fitting theoretical result to experiment measurement of attenuation and
linear scatter a t 10w amplitudes, a method introduced by Medwin (ICI??), de Jong and Hoff
(1993) obtained numericd values for the stiffness and loss parameters of the shell for the
agent Aibunex. A theoretically simpler approach was taken by Hoff (Hoff 1996; Hoff et al.
1996) who replaced the two phases (gas and shell) of the bubble with a single phase with an
effective buk rnodulus. The real and imaginary parts of Hoff's effective bulk rnodulus are
related to the shell stiffness and loss parameters, respectively. Both de Jong (1994) and Hoff
(1999) went on to include shell parameters obtained by these linear methods in nonlinear
scattering caiculations using the Rayleigh mode1 (equation 1.10). Building on the heuristic
approach of de Jong, Church (1995) developed a Rayleigh-like equation that incorporatecl a
continuous layer of incompressible, solid elastic matenal as the shell. Using Miller's (1981)
weakly nodinea. approximation, Church then derived explicit fomulae for fundamental
and second h m o n i c scattering cross sections that are dependent on shell parameters. So
Far, there doesn't seem to be my theoretical or heuristic models that account For acoustic
disniption in the literature. A theoretical description of shell disniption may need to take into
account that the shells on many agents are oniy a few molecules thick. This rnay present a
substantial challenge since the mechanics of molecular films is still an active area of reseach.
Granick (1999) noted that "when the thickness of a üquid film becomes comparable to
molecdar dimensions, classicd intuition based on continuum properties no longer applies."
This means that existing shell models based on the mechanics of solids or liquids may be
M c i e n t for the description of ultrasound contrast agents.
C W T E R 6. CONCLUSIONS
6.3.2 Evolution of the Bubble Sizes In Vivo
M e r injection into the bIood stream, the microbubbles undergo a number of changes that
affect theu performance as contrast agents. There are two processes by which the microbub-
bles are cleared fkom the blood stream. Microvarcular networks (especially in the lungs)
passively iîlter the larger bubbles. In addition, depending on the chemistry of the shell ma-
terid, the immune system may remove the microbubbles from the circulating blood. Since
typically the agent is injected into a peripheral vein and scanning is performed on the sys-
temic side of the circulation systern, the fùst microbubbles to appear in the image have
passed through the pulmonary system once. Within a minute, d i the bubbles will have
made multiple passages through the lungs. With each passage, some of the larger bubbles
are filtered by the capiUaRes. Unfortunately, the size distribution of microbubbles in vivo
cannot yet be measured reliably, therefore, the effects of lung filtration axe not yet quaatified.
However, the size distribution of lung capillaxies is known and a simple numerical method
for r n o d w g the size distribution of microbubbles after the lung passage has been proposed
(Bouakaz et al. 1998). Kupffer ceUs in the Iiver sinusoids actively scavenge and phagocy-
tose the microbubbles of several agents. Within a few hours of injection, the microbubbles
are collected in the liver parenchyrna. These bubbles can still scatter ultrasound efficiently.
Since Kupffer cells are present only in normal liver parenchyrna, the absence of contrast
has been suggested as an indication of liver tumours (Forsberg et al. 1995). At present, it
is not known how phagacytosis of rnicrobubbles depends on size, sheU materials and other
properties.
Since the nodinear scattering of contrast agent is dependent on the bubbie sizes,
CXU..PTER 6. C O ~ U S I O N S 115
the lack of quantitative information of an vivo size distribution limits, to some extent, the
appücation of the population mode1 to chicai imaging. Experimental methods to detennine
the evolution of the size distribution after the injection need to be developed.
6.4 Final Remarks
The field of microbubble contrast agents has corne of age, with rapid progress still aising
in the basic physics, detection met hods and clinical applications. The study of fundamental
mechanisms of nonlinear oscillation has not yet produced a tum-key solution to design and
optimize agent detection methods. Instead, the theoretical mode1 provided useful insights
and contributed to the posing of scientSc questions and the interpretations of experimental
results. A theoretical understanding of the basic acoustic behaviour of contrast agents is
expected to play an expanding role in dtrasound contrast Maging.
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