Dalgalar II

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    University of Cape Town

    Department of PhysicsPHY2014F

    Vibrations and Waves

    Andy BufflerDepartment of Physics

    University of Cape [email protected]

    Part 2

    Coupled oscillators

    Normal modes of continuous systemsThe wave equation

    Fourier analysis

    covering (more or less)

    French

    Chapters 2, 5 & 6

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    Problem-solving and homework

    Each week you will be given a take-home problem set to

    complete and hand in for marks ...

    In addition to this, you need to work through the followingproblems inFrench, in you own time, at home. You will not

    be

    asked to hand these in for marks. Get help from you friends, the

    course tutor, lecturer, ... Do not take shortcuts.Mastering these problems is a fundamental aspect

    of this course.

    The problems associated with Part 2

    are:

    2-2, 2-3, 2-4, 2-5, 2-6, 5-2, 5-8, 5-9, 6-1, 6-2, 6-6, 6-7, 6-10,

    6-11, 6-14

    You might find these tougher: 5-4, 5-5, 5-6, 5-7

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    The superposition of periodic motions

    Two superimposed vibrations of equal frequency

    1 1 0 1cos( )x A t = +

    2 2 0 2cos( )x A t = +

    combination can be written as

    0cos( )x A t = +

    Using complex numbers:0 1( )

    1 1

    j tz A e

    +=0 2( )

    2 2

    j tz A e

    +=1 2z z z= +

    { }0 1 2 1( ) ( )1 2j t jz e A A e + = +

    A A2

    A1

    0 1t +

    2 1

    2 1 =

    Phase differenceThen

    ( )2 2 1sin sinA A = and

    2 2 2

    1 2 1 2 2 12 cos( )A A A A A = + +

    French

    page 20

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    If we add two sinusoids of slightly different frequency and we observe beats

    x1x2

    x1

    +x

    2

    t

    t

    Superposed vibrations of slightly different frequency: Beats

    2cos t

    1 2

    cos cost t +1 2cos

    2

    t

    1 2

    2beatT

    =

    1cos t

    1 2 1 21 2cos cos 2cos cos

    2 2t t t t

    + + =

    1

    2

    French

    page 22

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    Combination of two vibrations at right angles

    1 1 1cos( )x A t = +2 2 2cos( )y A t = +

    ???

    Write and1 0cos( )x A t=

    Consider case where frequencies are equal and let initialphase difference be

    2 0cos( )y A t = +

    Case 1 : 0 = 1 0cos( )x A t=

    2 0cos( )y A t=

    2

    1

    Ay x

    A= Rectilinear motion

    2 = 1 0cos( )x A t=

    2 0 2 0cos( 2) sin( )y A t A t = + =

    Case 2 :

    2 2

    2 2

    1 2

    1x yA A

    + = Elliptical path inclockwise direction

    French

    page 29

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    Case 3 : = 1 0cos( )x A t= 2

    1

    Ay xA

    =

    Combination of two vibrations at right angles 2

    2 0 2 0cos( ) cos( )y A t A t = + =

    3 2 = 1 0cos( )x A t=2 0 2 0cos( 3 2) sin( )y A t A t = + = +

    Case 4 :

    2 2

    2 2

    1 21

    x y

    A A + = Elliptical path inanticlockwise direction

    4 = 1 0cos( )x A t=

    2 0cos( 4)y A t = +

    Case 5 :

    Harder to see use a graphical approach

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    Superposition of simple

    harmonic vibrations at

    right angles with an initialphase difference of 4

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    Superposition of two perpendicular simple

    harmonic motions of the same frequency forvarious initial phase differences.

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    Abbreviated construction for the superposition of

    vibrations at right angles

    see French page 34.

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    Perpendicular motions with different frequencies: Lissajous figures

    See French page 35.

    Lissajous figures for

    with various

    initial phase differences.

    2 12 =

    = 0 4 3 42

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    2 1:

    1:1

    1:2

    2:3

    1:3

    3:4

    5:6

    4:5

    3:5

    = 0 4 3 42

    Lissajous figures

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    Coupled oscillators

    When we observe two weakly coupled identical oscillators

    A and B, we see:

    t

    t

    xA

    xB

    these functions arise mathematically from the addition of twoSHMs

    of similar frequencies

    so what are

    these two SHMs?

    These two modes are known as normal modes which are states

    of the system in which all parts of the system oscillate with SHM

    either in phase or in antiphase.

    French

    page 121

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    t

    t

    A B

    xA

    xB

    Coupled oscillators

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    The double mass-spring oscillator

    m

    Axk

    m

    Bx k

    Individually we know that andA Amx kx= B Bmx kx=

    For both oscillators:0

    k

    m

    =

    Now add a weak coupling force:

    m

    Axk

    m

    Bx kck

    For mass A: ( )A A c B Amx kx k x x= +

    or where ,2 20 ( )A A B Ax x x x= + 2

    0k

    m = 2 ck

    m =

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    2 2

    0 ( )A A B Ax x x x= +

    The double mass-spring oscillator 2

    For mass A:

    For mass B:2 2

    0( )

    B B B Ax x x x=

    two coupled differential equations how to solve ?Adding them:

    22

    02( ) ( )

    A B A B

    dx x x x

    dt+ = +

    Subtract B from A:2

    2 2

    02( ) ( ) 2 ( )

    A B A B A Bd x x x x x xdt

    =

    Define two new variables:1 A Bq x x= +

    2 A Bq x x=

    Then and2

    21 0 12

    d qqdt =

    2

    2 22 0 22 ( 2 )d q

    qdt = +

    called normalcoordinates

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    The double mass-spring oscillator 3

    The two equations are now decoupled

    221

    12 s

    d qq

    dt

    =

    Write 222

    22 f

    d qq

    dt=

    2 2

    0s =

    2 2 2

    02

    f = +

    s

    = slow

    f

    = fast

    which have the solutions:

    1 1cos( )

    sq C t = +

    2 2cos( )fq D t = +

    Since and 2 A Bq x x=

    We can write and

    1 A Bq x x= +

    ( )

    1

    1 22A

    x q q= +( )

    1

    1 22B

    x q q=

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    The double mass-spring oscillator 4

    1 2

    cos( ) cos( )2 2A s f

    C Dx t t = + + +

    Then1 2cos( ) cos( )

    2 2B s f

    C Dx t t = + +

    SoxA

    andxB

    have been expressed as the sum and difference of

    two SHMs

    as expected from observation.

    C,D, 1

    and 2

    may be determined from the initial conditions.

    whenxA

    =xB

    ,then q2

    = 0

    there is no contribution from the

    fast mode and the two masses move in phase

    the coupling spring

    does not change length and has no effect on the motion 0s =

    whenxA

    = xB

    ,then q1

    = 0

    there is no contribution from the

    slow mode

    the coupling spring gives an extra force

    each mass

    experiences a force giving( )2c

    k k x +

    2 2

    02= +

    2 2 cf

    k k

    m

    +

    =

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    The double mass-spring oscillator 5

    symmetric mode antisymmetric

    mode mixed mode

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    The double mass-spring oscillator 6

    We now have a system with two natural frequencies, and

    experimentally find two resonances.

    Frequency

    Amplitude

    F h

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    Pitch and bounce oscillator

    d

    Axk

    m

    Bx

    L

    k

    Two normal modes (by inspection):

    Bouncing

    A Bx x=

    Restoring force = 2kx2

    2 2

    d x

    m kxdt = Pitching

    A B

    x x= Ax

    Bx Centre of mass stationary

    2

    bounce

    2k

    m =

    I =

    21 12 12

    ( )kd d mL = 2

    26kdmL

    =2

    2

    pitch 26k dm L

    =

    French

    page 127

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    N= 2

    ( )1 0 01

    2 sin2 2 1

    = =

    +

    ( )2 0 022 sin 3

    2 2 1 = =+

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    N

    = 4

    N

    = 3

    French

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    N-coupled oscillators

    fixed fixedTension T

    l

    1 2 3 p1 p p+1 N

    consider transverse displacements that are small.

    Each bead has mass m

    1 2 3 p1 p p+1 N

    1p

    p

    Transverse force on pth particle:1sin sinp p pF T T = +

    1 1p p p py y y yT T

    l l

    + = +

    for small

    y

    French

    page 136

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    N-coupled oscillators 2

    2

    1 12p p p p p

    p d y y y y yF m T Tdt l l

    +

    = = +

    ( )

    2

    2 2

    0 0 1 12 2 0p

    p p p

    d y

    y y ydt + + =

    where ,20

    T

    ml = p

    = 1, 2

    N

    a set ofN

    coupled differential equations.

    Normal mode solutions: sinp py A t=

    Substitute to obtainN

    simultaneous equations

    ( ) ( )2 2 20 0 1 12 0p p pA A A + + =

    or2 21 1 0

    2

    0

    2p p

    p

    A AA

    + +=

    i 3

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    N-coupled oscillators 3

    From observation of physical systems we expect sinusoidalshape functions

    of the form sinpA C p=

    Substitute into

    2 2

    1 1 02

    0

    2p p

    p

    A A

    A

    +

    +=

    And apply boundary conditions and0 0A = 1 0NA + =

    and

    n

    = 1, 2, 3,

    N

    (modes)

    ( )02 sin 2 1nn

    N

    = +

    find that1

    n

    N

    =

    +

    There areN modes: sin sin sin1

    pn pn n n n

    pny A t C t

    N

    = =

    +

    N l d ill t 4

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    02

    n

    0 1 2 3 N+1 n

    ( )02 sin 2 1nn

    N

    = +

    N-coupled oscillators 4

    For smallN:

    N l d ill t 5

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    Forn

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    N

    coupled oscillators haveN

    normal modes and henceN

    resonances

    response

    N-coupled oscillators 6

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    Continuous systems

    Continuous systems

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    Continuous systems

    Consider a string stretched between two rigid supports

    x = 0 x =L

    tension T

    String has mass m

    and mass per unit length m L=

    Suppose that the string is disturbed in some way:

    y

    x

    The displacementy

    is a function ofx

    and t : ( , )y x t

    TNormal modes of a stretched string

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    T

    T

    +

    y

    x xx x+

    Consider the forces on a

    small length of string

    Restrict to small amplitude disturbances then is small andcos 1 = sin tan yx

    = = =

    The tension T

    is uniform throughout the string.

    Net horizontal force is zero: cos( ) cos 0T T + =

    Vertical force: sin( ) sinF T T = +

    Thenx x x

    y yF T Tx x

    + =

    g

    French

    page 162

    Normal modes of a stretched string 2

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    x x x

    y yF T T

    x x+

    =

    Use( ) ( )dg g x x g x

    dx x

    + =

    Then2

    2

    yF T x

    x=

    or ( )

    2 2

    2 2

    y y

    x T xt x

    =

    giving

    2 2

    2 2

    y y

    x T t

    =

    Check: has the

    dimensions

    T21 v

    Then is the speed at which awave propagates along

    the string see later

    v T =

    Write2 2

    2 2 2

    1y y

    x v t

    =

    One dimensional wave equation

    Normal modes of a stretched string 2

    : mass per unit length

    Normal modes of a stretched string 3

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    Look the standing wave (normal mode) solutions

    Normal mode: all parts of the system move in SHM at the

    same frequency

    Write: ( , ) ( )cosy x t f x t=( )f x is the shape

    function

    substitute into wave equation

    2 2

    2 2( , ) ( ) cosy x t d f x tx dx

    =

    ( )

    22

    2

    ( , )

    ( ) cos

    y x t

    f x tt

    =

    22

    2 2

    ( ) 1cos ( )cos

    d f xt f x t

    dx v =

    which must be true for all t

    then

    2 2

    2 2 ( )d f

    f xdx v

    =

    No a odes o a st etc ed st g 3

    Normal modes of a stretched string 4

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    2 2

    2 2 ( )

    d f

    f xdx v

    =

    which has the same form as the eq. of SHM:2

    2

    02

    d xx

    dt=

    has general solution:0sin( )x A t = +

    Thus we must have: ( ) sinf x A x

    v

    = +

    Apply boundary conditions: y

    = 0 at x = 0 and x

    =L

    (0) 0f = and ( ) 0f L =

    x

    = 0,f

    =0 : 0 sin 0A

    v

    = +

    i.e.

    0 sin Lv

    =

    0 =

    x = L,f =0 : L nv

    =i.e. n = 1,2,3,

    g

    Normal modes of a stretched string 5

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    n

    n v

    L

    =Write n = 1,2,3,( ) sin sinn n

    x n v n xf x A A

    v L L

    = =

    Therefore

    shape function, or eigenfunction

    x

    = 0

    x

    =L

    n = 1

    n = 3n

    = 2

    n = 5n

    = 4

    ( )1( ) sinf x A x L=( )2( ) sin 2f x A x L=

    ( )3( ) sin 3f x A x L=

    ( )4( ) sin 4f x A x L=

    ( )5( ) sin 5f x A x L=

    1

    v L =

    3 3 v L =

    2 2 v L =

    5 5 v L =

    4 4 v L =

    g

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    Normal modes of a stretched string

    n

    = 1

    n

    = 2

    n

    = 3

    n = 4

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    Normal modes of a stretched string 6

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    Full solution for our standing waves:

    ( , ) sin cosn nn x

    y x t A tL

    =

    n

    n v

    L

    =

    The mode frequencies are evenly spaced:1n n =

    n

    0 1 2 3 n

    3

    2

    1

    (recall the beaded string)

    This continuum approach breaks

    down as the wavelength approaches

    atomic dimensions

    also if there is

    any stiffness in the spring whichadds an additional restoring forcewhich is more pronounced in the

    high frequency modes.

    Normal modes of a stretched string 7

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    All motions of the system can be made up from thesuperposition of normal modes

    1

    ( , ) sin cos( )n n nn

    n xy x t A t

    L

    =

    = +

    with n

    n v

    L

    =

    Note that the phase angle is back since the modes may

    not be in phase with each other.

    Whispering galleries

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    Whispering galleries

    best example is the inside

    dome of St. Pauls cathedral.

    If you whisper just inside the

    dome, then an observer close to

    you can hear the whisper

    coming from the oppositedirection

    it has travelled

    right round the inside of the

    dome.

    Longitudinal vibrations of a rodFrench

    page 170

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    x x x+

    x x + + + x +

    1F 2F

    section of massive rod

    section is displaced and stretched

    by an unbalanced force

    Average stress =x

    Average strain = Y

    x

    Y: Youngs modulus

    stress at = (stress atx) +x x+ (stress)

    xx

    page 170

    Longitudinal vibrations of a rod 2

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    If the cross sectional area of the rod is

    1F Yx

    =

    2

    2 2F Y Y x

    x x

    = +

    and

    2

    1 2 2F F Y x ma

    x

    = =

    2 2

    2 2Y x xx t

    =

    or2 2

    2 2

    x Y t

    =

    2 2

    2 2 2

    1

    x v t

    =

    Yv =

    Longitudinal vibrations of a rod 3

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    Apply boundary conditions: one end fixed and the other free

    x =L :x

    = 0 : i.e. 0 =

    n

    = 1,2,3,

    ( , ) ( )cosx t f x t =Look for solutions of the type:

    (0, ) 0t =

    0F Yx

    = =

    ( ) sinf x A xv

    = +

    where

    then cos 0L

    v

    =

    or ( )12L nv

    =

    ( ) ( )1 12 2n

    n v n Y

    L L

    = =The natural angular frequencies

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    x = 0 x =Ln

    = 1

    n = 3

    n

    = 2

    n

    = 5

    n

    = 4

    12

    Y

    L

    =

    232

    YL

    =

    3

    5

    2

    Y

    L

    =

    Normal modes for different boundary conditions

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    45n

    = 1 n

    = 2 n

    = 3

    Simplysupported

    Clampedone end

    Free bothends

    Clampedboth ends

    The elasticity of a gasl

    French

    page 176

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    A , p Bulk modulus:dp

    K VdV=

    Kinetic theory of gases: Pressure

    2 21

    rms rms3 3

    m

    p v vAl= =If then

    21rms2k

    E mv=2

    3

    kEpA l

    =

    Now move piston so as to compress the gas work done on

    gas:

    kW pA l E = =

    Then ( )2

    2 2 2 5( )

    3 3 3 3

    kk

    E l l lp E pA l p p

    A l A l A l l

    = = =

    adiabatic

    5

    3

    pK V p

    V

    = =

    giving

    and1.667K p

    v = =

    Sound waves in pipesFrenchpage 174

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    A sound wave consists of a series of compressions and

    rarefactions of the supporting medium (gas, liquid, solid)

    In this wave individual molecules move longitudinally with

    SHM. Thus a pressure maximum represents regions in which themolecules have approached from both sides, receding from the

    pressure minima.

    wave propagation

    p g

    Longitudinal wave on a spring

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    Standing sound waves in pipes

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    Pressurep

    p0

    Flow

    velocity u

    0

    x

    x

    x

    x

    0 :t=

    2 :t T=p

    u

    Standing sound waves in pipes 2

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    Consider a sound wave in a pipe. At the closed end the flow

    velocity is zero (velocity node, pressure antinode).At the open end the gas is in contact with the atmosphere,

    i.e.p

    =p0

    (pressure node and velocity antinode).

    p

    u

    p0

    0

    pressure node

    velocity antinode

    pressure antinode

    velocity node

    Open end Closed end

    Standing sound waves in pipes 3

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    Pipe closed at

    both ends

    Pipe open at

    both ends

    Pipe open at

    one end

    n n vL =

    2 2

    n nvL

    f

    = =

    2

    nvf

    L=

    ( ) ( )2 1 2 1

    4 4

    n n vL

    f

    = =

    ( )2 1

    4

    n vf

    L

    =

    ( )2 12

    nn v

    L =

    Sound

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    Audible sound is usually a longitudinal compression wave in air towhich the eardrum responds.

    Velocity of sound (at NTP) ~ 330 m s-1

    By considering the transport of energy by a compression wave,

    can show that 2 2 22 mP f Avs =

    whereA

    is cross sectional area of air column andsm

    is

    maximum displacement of air particle in longitudinal wave

    Then intensity = 2 2 22 mP

    f vsA

    = unit: W m-2

    Sound 2

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    The human ear detects sound from ~10-12

    W m-2

    to ~1 W m-2

    use a logarithmic scale forI :

    10

    0

    10logI

    I

    =

    decibels

    whereI0

    = reference intensity

    = 10-12

    W m-2

    Intensity level or loudness:

    Musical sounds

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    Waveforms from real musical instruments are complex, and maycontain multiple harmonics, different phases, vibrato, ...

    Pitch is the characteristic of a sound which allows sounds to be

    ordered on a scale from high to low (!?). For a pure tone, pitch

    is

    determined mainly by the frequency, although sound level may

    also change the pitch. Pitch is a subjective sensation and is a

    subject in psychoacoustics.

    The basic unit in most musical scales is the octave. Notes judged

    an octave apart have frequencies nearly (not exactly) in the ratio2:1. Western music normally divides the octave into 12 intervals

    called semitones ... which are given note names (A through G withsharps and flats) and designated on musical scales.

    Musical sounds ...2

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    Timbre is used to denote tone quality or tone colour of asound and may be understood as that attribute of auditorysensation whereby a listener can judge that two sounds are

    dissimilar using any criteria other than pitch, loudness or

    duration. Timbre depends primarily on the spectrum of the

    stimulus, but also on the waveform, sound pressure and

    temporal characteristics of the stimulus.

    One subjective rating scale for timbre (von Bismarck, 1974)

    dull

    compact

    full

    colourful

    sharp

    scattered

    empty

    colourless

    Two dimensional systems Frenchpage 181

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    the membrane has mass per unit area ,

    and a surface tension S

    which gives a force Sl

    perpendicular to a length l in the surface

    y

    x

    y

    x

    The forces on the shaded

    portion are

    Sx

    Sx

    SySy

    Consider an elastic

    membrane clamped

    at its edges

    Two dimensional systems 2

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    If the membrane is displaced

    from thez

    = 0 plane then a

    cross section through the

    shaded area shows:

    +

    z

    x xx x+

    Sy

    Sy

    looks exactly like the case of the stretched string.2

    2zS y xx The transverse force on the element will be

    And if we looked at a cross section perpendicular to this

    the transverse force will be2

    2

    zS x y

    y

    Two dimensional systems 3

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    The mass of the element is .x y

    Thus2 2 2

    2 2 2

    z z zS y x S x y x y

    x y t

    + =

    or2 2 2

    2 2 2

    z z z

    x y S t

    + =

    a two dimensional wave equation

    with the wave velocity Sv

    =

    L k f l d l i f h f

    Two dimensional systems 4

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    ( , , ) ( ) ( )cosz x y t f x g y t=2 2

    2 2( )cos

    z d fg y t

    x dx

    =

    ( )2

    2

    2( ) ( ) cos

    zf x g y t

    t =

    Look for normal mode solutions of the form:

    2 2

    2 2( )cos

    z d gf x t

    y dy

    =

    2 2

    2 2( )cos ( )cosd f d g

    g y t f x tdx dy + =2

    2( ) ( )cosf x g y t

    v

    2 2 2

    2 2 2

    1 1d f d g

    f dx g dy v

    + = i.e.

    In a similar fashion to the 1D case, find

    1

    1( ) sinnx

    n xf x A

    L

    =

    and2

    2( ) sinny

    n yg y B

    L

    =

    Two dimensional systems 5

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    then1 2 1 2

    1 2,( , , ) sin sin cosn n n n

    x y

    n x n yz x y t C tL L

    =

    1 2

    22

    1 2,n n

    x y

    n v n v

    L L

    = +

    where the normal mode frequencies are

    e.g. for a membrane having sides 1.05L and 0.95L

    then1 2

    2 21 2

    ,1.05 0.95

    n n

    n nv

    L

    = +

    Normal modes of a rectangular membrane

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    up

    down1,1

    2,1 2,2

    3,1 3,2

    Normal modes of a circular membrane

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    1,0 2,0 3,0

    1,1 2,1 2,2

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    Modes of vibration of a 38 cm cymbal. The first 6 modes

    resemble those of a flat plate ... but after that the resonances

    tend to be combinations of two or more modes.

    Normal modes of a circular drum

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    Chladni plates

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    Soap films

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    Holographic interferograms

    of the top and bottom plates

    of a violin at several resonances.

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    Holographic interferograms

    of a classical guitar top

    plate at several resonances.

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    Holographic interferograms

    showing the vibrations of a 0.3 mm

    thick trombone driven acoustically at 240 and 630 Hz.

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    Time-average hologram interferograms

    of inextensional

    modes in a C5

    handbell

    Normal modes of a square membrane

    v2n area per point =

    2v

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    one point per

    normal mode

    1 2

    2 2

    1 2,

    2 2n n

    n v n vf

    L L

    = +

    12

    v

    L

    22

    v

    L

    32

    v

    L

    4 2

    v

    L

    0

    12

    v

    L 2 2

    v

    L 3 2

    v

    L 4 2

    v

    L 5 2

    v

    L00 1 2 3 4 5

    0

    1

    2

    3

    4

    4,3f

    1n

    Normal modes having the same frequency are said to be degenerate

    2L

    Normal modes of a square membrane for large n1 and n2

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    1

    n

    2ndf

    f

    area =

    2

    2

    v

    L

    area per mode =

    14(2 )f df

    Number of modes with

    frequencies betweenf

    and (f+ df) =

    2

    14

    2(2 )

    Lf df

    v

    2

    2

    2 L f df

    v

    =

    Three dimensional systems

    Consider some quantity which depends on x y z and t

    French

    page 188

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    Consider some quantity

    which depends onx

    , y , z

    and t

    ,

    e.g. the density of air in a room.

    In three dimensions:2 2 2 2

    2 2 2 2 2

    1

    x y z v t

    + + =

    which can be written:2

    2

    2 2

    1

    v t

    =

    The solutions for a rectangular enclosure:

    1 2 3

    22 2

    31 2, ,n n n

    x y z

    n vn v n vL L L

    = + +

    and for a cube: 1 2 32 2 2

    , , 1 2 3n n n

    v

    n n nL

    = + +

    How many modes are there with frequencies in the range

    Three dimensional systems 2

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    f and (f+ df) ?Set up an imaginary cubic lattice with spacing 2v L2n

    1n

    3n

    df

    f

    and consider positive frequencies only.

    Volume of shell =21

    8(4 )f df

    3

    2vL

    Volume per mode =

    Number of modes with

    frequencies betweenf

    and (f+ df) =

    3

    218

    2(4 )

    Lf df

    v

    3 2

    34 L f dfv=

    Number of modes with 24 V f df =

    Three dimensional systems 3

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    frequencies betweenf and (f+ df) 3v=

    holds for any volume V

    provided its dimensions are much

    greater than the wavelengths involved.

    need to multiply by a factor of 2 when dealing withelectromagnetic radiation (2 polarization states)

    Ultraviolet catastrophe for blackbody radiation

    Equipartition

    theorem: in thermal equilibrium each mode has an

    average energy in each of its two energy stores

    Hence, energy density of radiation in a cavity:

    12 Bk T

    ( )2

    123

    42 2

    V f df df kT

    c

    =

    or

    2

    3

    8 fkTc

    = f

    experiment

    !?

    Planck was able to show, effectively by

    assuming that energy was emitted an

    absorbed in quanta of energy hf that the

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    absorbed in quanta of energy hf

    , that the

    average energy of a cavity mode was not kT

    but1hf kT

    hf

    e

    where Plancks constant h

    = 6.67

    10-34

    J K-1

    Then

    2

    3

    8

    1hf kTf df hf

    df c e

    =

    which agrees extremely well with experiment.

    energy

    density

    no. of

    modes inrangef

    tof

    +df

    average

    energy permode

    Plancks law

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    Introduction to Fourier methods

    We return to our claim that any physically observed shape

    French

    page 189

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    y p y y p

    function of a stretched string can be made up from normal

    mode shape functions.

    x

    ( )f x

    i.e.1

    ( ) sinnn

    n xf x B

    L

    =

    =

    a surprising claim

    ?

    first find

    n

    multiply both sides by

    and integrate over the range x

    = 0 to x = L

    1

    sin

    n x

    L

    1 1

    10 0( )sin sin sin

    L L

    n

    n

    n x n x n xf x dx B dxL L L

    =

    =

    1 1( )sin sin sin

    L L

    n

    n x n x n xf x dx B dx

    =

    Fourier methods 2

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    10 0 nL L L=

    If the functions are well behaved, then we can re-order things:

    1 1

    10 0

    ( )sin sin sin

    L L

    n

    n

    n x n x n xf x dx B dxL L L

    = =

    [n1

    is a particular integer and n

    can have any value between 1 and .]

    Integral on rhs:

    ( ) ( )1 110 0

    1sin sin cos cos2

    L L

    n n x n n xn x n x dx dxL L L L

    + =

    Fourier methods 3

    Both (n1 + n) and (n1 n) are

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    integers, so the functions

    on the intervalx

    = 0 toL

    must look like from which it is evident that

    ( )1cos

    n n x

    L

    ( )1

    0

    cos 0

    L n n xdx

    L

    =

    Except for the special case when n1

    and n are equal then ( )1

    cos 1n n x

    L

    =

    and

    ( )1

    0

    cos

    L n n xdx L

    L

    =

    Fourier methods 4

    Thus all the terms in the summation are zero, except for the

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    single case when n1

    = n i.e.

    1 2n

    LB=

    ( ) ( )1

    1 11

    0 0

    1( )sin cos cos

    2

    L L

    n

    n n x n n xn xf x dx B dx

    L L L

    + =

    1

    1

    0

    2 ( )sin

    L

    n n xB f x dxL L

    =

    i.e.

    We have found the value of the coefficient for some

    particular value ofn1

    the same recipe must work for any

    value, so we can write:

    0

    2( )sin

    L

    n

    n xB f x dx

    L L

    =

    Fourier methods 5

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    The important property we have used is that the functions

    and

    are orthogonal over the intervalx

    = 0 tox

    =L.

    i.e.

    1sinn x

    L

    sinn x

    L

    1

    0

    sin sin

    Ln x n x

    dxL L

    =

    10 if n n

    1if2

    L n n=

    Read French pages 195-6

    Fourier methods 6

    The most general case (where there can be nodal or

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    g (

    antinodal

    boundary conditions atx

    = 0 andx

    =L) is

    0

    1( ) cos sin2

    n n

    n

    A n x n xf x A BL L

    =

    = + +

    where

    0

    2

    ( )sin

    L

    n

    n x

    B f x dxL L

    =

    0

    2

    ( )cos

    L

    n

    n x

    A f x dxL L

    =

    Fourier methods 7

    One of the most commonly encountered uses of Fourier methods is

    the representation of periodic functions of time in terms of sine

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    and cosine functions

    Put2

    T

    =

    This is the lowest frequency in

    clearly there are

    higher frequencies

    by the same method as before, write

    ( )f t

    0

    1

    2 2( ) cos sin

    2n n

    n

    A nt nt f t A B

    T T

    =

    = + +

    0

    1cos sin2

    n n

    n

    AA n t B n t

    == + +

    where and ( )0

    2( )sin

    T

    n f t n t dt

    T

    = ( )0

    2( )cos

    T

    nA f t n t dt

    T

    =

    T( )f t

    t

    Waveforms of ...

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    a flute

    a clarinet

    an oboe

    a saxophone

    Fast Fourier transform experiments, 10 March 2008

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    Fast Fourier transform experiments, 10 March 2008

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    Fast Fourier transform experiments, 10 March 2008

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    Fast Fourier transform experiments, 10 March 2008

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    Fast Fourier transform experiments, 10 March 2008

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    Odd functions

    An odd periodic function ( ) ( )f t f t =

    h

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    where 2 2T t T