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Narrowing of hysteresis of cubic-tetragonal martensitic transformation by weak axialstressing of ferromagnetic shape memory alloyAnna Kosogor Citation: Journal of Applied Physics 119, 224903 (2016); doi: 10.1063/1.4953868 View online: http://dx.doi.org/10.1063/1.4953868 View Table of Contents: http://scitation.aip.org/content/aip/journal/jap/119/22?ver=pdfcov Published by the AIP Publishing Articles you may be interested in Effect of niobium addition on the martensitic transformation and magnetocaloric effect in low hysteresisNiCoMnSn magnetic shape memory alloys Appl. Phys. Lett. 105, 231910 (2014); 10.1063/1.4903494 Microstructures and magnetostrictive strains of Fe-Ga-Ni ferromagnetic shape memory alloys J. Appl. Phys. 113, 17A303 (2013); 10.1063/1.4793609 Martensitic and magnetic transformation in Mn50Ni50−xSnx ferromagnetic shape memory alloys J. Appl. Phys. 112, 083902 (2012); 10.1063/1.4758180 Martensitic transformation and magnetic field-induced strain in Fe–Mn–Ga shape memory alloy Appl. Phys. Lett. 95, 082508 (2009); 10.1063/1.3213353 Magnetization rotation and rearrangement of martensite variants in ferromagnetic shape memory alloys Appl. Phys. Lett. 90, 172504 (2007); 10.1063/1.2730752
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Narrowing of hysteresis of cubic-tetragonal martensitic transformationby weak axial stressing of ferromagnetic shape memory alloy
Anna Kosogora)
Institute of Magnetism, Kyiv 03142, Ukraine and National University of Science and Technology “MISiS,”Moscow 119049, Russia
(Received 24 December 2015; accepted 2 June 2016; published online 14 June 2016)
An influence of axial mechanical stress on the hysteresis of martensitic transformation and ordinary
magnetostriction of ferromagnetic shape memory alloy has been described in the framework of a
Landau-type theory of phase transitions. It has been shown that weak stress can noticeably reduce
the hysteresis of martensitic transformation. Moreover, the anhysteretic deformation can be observed
when the applied mechanical stress exceeds a critical stress value. The main theoretical results were
compared with recent experimental data. It is argued that shape memory alloys with extremely low
values of shear elastic modulus are the candidates for the experimental observation of large anhyste-
retic deformations. Published by AIP Publishing. [http://dx.doi.org/10.1063/1.4953868]
I. INTRODUCTION
Ferromagnetic shape memory alloys (FSMAs) undergo
both the ferromagnetic ordering and the martensitic transfor-
mation (MT) on their cooling.1–3 The FSMAs are character-
ized by a number of unique features. In particular, giant (up
to 10%) deformations under a very small (�2 MPa) mechani-
cal stress or a moderate (� 5 kOe) magnetic field attract
much attention of researchers and engineers.3–8 These effects
are known as the superelasticity or magnetic shape memory,
respectively.
It is of common knowledge that the hysteresis is one of
the basic features of MTs, which are the first-order phase
transitions. The manufacturing and the scientific study of the
alloys with small hysteresis of MTs are among the modern
trends in materials science.9–11 In particular, an unusual
anhysteretic stress–strain behavior characterized by a giant
nonlinear deformation (more than 12%) was observed exper-
imentally for the Ni-Fe(Co)-Ga alloy above certain critical
temperature T�, whereas stress–strain loops showing a pro-
nounced hysteresis were obtained below this temperature.12
It has been argued that the reduction of hysteresis can occur
when the temperature of the deformed alloy exceeds T�,because this temperature corresponds to the critical point in
the stress–temperature phase diagram.12 In Ref. 13, it has
been shown experimentally that the temperature hysteresis
of MT in the Fe-Pd alloy decreases by one order of magni-
tude (or even more) with an increase in the absolute stress
value from 5 MPa to 40 MPa. Moreover, vanishing of MT
strain, which is a jump of strain value, was observed when
stress applied to the cooled/heated specimen was larger than
the critical stress corresponding to the critical point of the
phase diagram.13 It should be noted that the existence of
the critical point of MT was predicted much earlier using
the Landau theory of phase transitions,14 but experimental
evidences of this fact were obtained only recently for
Ni-Fe(Co)-Ga and Fe-Pd alloys.12,13
In the present article, Landau theory is used to demon-
strate a possibility of the reduction and disappearance of
temperature hysteresis under a small axial stress applied to
the representative FSMA with physical properties inherent
to Ni-Mn-Ga shape memory alloys. The stress-induced
changes of the MT temperature, MT strain, Young’s modu-
lus, and ordinary magnetostriction of the FSMA, as well as
the coordinates of the critical point at the phase diagram, are
evaluated. The conditions providing the observation of
anhysteretic deformations of a shape memory alloy (SMA)
are formulated.
II. QUANTITATIVE THEORY OF MARTENSITICTRANSFORMATIONS
Landau theory of phase transitions provides a consistent
theoretical description of cubic-tetragonal and cubic-
rhombohedral MTs.14–16 The basic properties of the alloys
undergoing the cubic-orthorhombic MTs are satisfactorily
described by this theory if the shape of the orthorhombic unit
cell of the crystal lattice is rather close to tetragonal. The
influence of the stress on the basic properties of SMAs
exhibiting the cubic-tetragonal and cubic-rhombohedral MTs
is fairly similar, so the case of cubic-tetragonal MT will be
considered below, for the sake of definiteness.
Landau theory describing the cubic-tetragonal marten-
sitic transformations starts from the following expression for
Gibbs potential:
G ¼ c2ðu22 þ u2
3Þ=2þ a4u3ðu23 � 3u2
2Þ=3
þ b4ðu22 þ u2
3Þ2=4� ðrðeff Þ
2 u2 þ rðeff Þ3 u3Þ=6; (1)
where
u2 ¼ffiffiffi3pðexx � eyyÞ; u3 ¼ 2ezz � eyy � exx; (2)
are the order parameter components of the cubic–tetragonal
MT, eik are the strain tensor components, and the values of
the effective stress rðeff Þ2;3 are expressed through the stress
components in the same way as the values u2;3 are related toa)E-mail: [email protected]
0021-8979/2016/119(22)/224903/7/$30.00 Published by AIP Publishing.119, 224903-1
JOURNAL OF APPLIED PHYSICS 119, 224903 (2016)
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the strain components. The effective stress is a sum of me-
chanical stress applied to the alloy and magnetoelastic stress
rðeff Þik ¼ rðmeÞ
ik þ rik: (3)
The magnetically induced (magnetoelastic) stress rðmeÞik is
strictly interrelated with ordinary magnetostriction and
appears during ferromagnetic ordering of alloy specimen
(see Refs. 8 and 17 and references therein). The coefficients
c2; a4; and b4 are linear combinations of second-, third-, and
fourth-order elastic modules introduced in Ref. 14.
The equilibrium states of the elastically deformed single
crystal can be determined from the minimum conditions for
Gibbs potential (Eq. (1)). These conditions were analyzed in
Ref. 14. The results obtained are briefly mentioned below
and used then for the illustration of basic properties of the
axially stressed shape memory alloys.
According to Landau theory, the coefficient c2 � c2ðTÞinvolved in Eq. (1) is an increasing linear function of temper-
ature. The equilibrium values of deformations are prescribed
by the conditions @G=@u2 ¼ @G=@u3 ¼ 0, which result in
the equation system
c2ðTÞu2 � 2a4u2u3 þ b4u2 u22 þ u2
3
� �� rðeff Þ
2 =6 ¼ 0; (4)
c2ðTÞu3 þ a4ðu23 � u2
2Þ þ b4u3 u22 þ u2
3
� �� rðeff Þ
3 =6 ¼ 0: (5)
In the case of a zero effective stress, this system has solu-
tions that correspond to the cubic phase and three variants
of tetragonal phase with four-fold symmetry axes oriented in
x-, y-, and z-directions, respectively.
For the sake of certainty, the phase transition to z-variant
of tetragonal phase may be considered. When the alloy spec-
imen is stressed in [001] or [110] directions, the condition
exx ¼ eyy is fulfilled and the value rðeff Þ2 is equal to zero. In
this case, Eq. (4) has a solution u2 ¼ 0 and Equation (5) is
reduced to the form
u3 c2ðTÞ þ a4u3 þ b4u23
� �� rðeff Þ
3 =6 ¼ 0; (6)
where the order parameter of cubic-tetragonal MT is related
to the lattice parameters of a tetragonal lattice, cðTÞ and
aðTÞ, and to the transformation strain, eM, as u3ðTÞ¼ 2½cðTÞ=aðTÞ � 1� � 3eM. If the effective stress is equal to
zero, the order parameter is equal to zero in the austenitic
(cubic) phase and is expressed as
uð0Þ3 ðTÞ ¼ �ða4=2b4Þð1þ
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1� c2ðTÞ=ct
pÞ (7)
in the martensitic phase (ct � a24=4b4). If the effective stress
is not equal to zero, Equation (6) does not have the solution
u3 ¼ 0, which corresponds to a cubic phase. It means that
the effective stress rðeff Þ3 produces the elastic strain that
reduces the cubic symmetry of the lattice to a tetragonal one.
The MT in an elastically strained lattice is not accompanied
by the symmetry reduction and is referred to as the isomor-
phic (tetragonal-tetragonal) first-order phase transition.
The study of the extremum of potential Eq. (1) enabled
the construction of stress–temperature phase diagrams for
the shape memory alloys undergoing temperature-induced or
stress-induced MTs. This diagram was constructed in Ref. 14.
It was shown that the axially compressed high-temperature
(austenitic) phase is stable if
rðeff Þzz > rLAðTÞ ¼ �16c2
t ½1� RðTÞ�2½1þ 2RðTÞ�=9a4; (8)
where RðTÞ ¼ ½1� 3c2ðTÞ=4ct�1=2and rðeff Þ
zz ¼ rzz þ rðmeÞzz .
The low-temperature (martensitic) phase is stable when
rðeff Þzz < rLMðTÞ ¼ �16c2
t ½1þ RðTÞ�2½1� 2RðTÞ�=9a4: (9)
(Note that the compressive stress is negative.) The inequal-
ities (8) and (9) mean that the plots of the functions rLAðTÞand rLMðTÞ represent the lability lines of austenitic and mar-
tensitic phases at the stress–temperature phase diagram. On
the other hand, the temperatures T2ðrðeff Þzz Þ and T1ðrðeff Þ
zz Þ are
the solutions of the equations rðeff Þzz ¼ rLAðTÞ and
rðeff Þzz ¼ rLMðTÞ, respectively. These temperatures bound the
stability ranges of two phases in the axially stressed alloy
specimen. The austenitic phase is stable if T > T2, while the
martensitic one is stable if T < T1. Equations (8) and (9)
show that the lability lines cross each other if the condition
RðTÞ ¼ 0 is fulfilled. The critical stress determined from this
condition is expressed through the shear modulus, C0ðT1Þ,and lattice parameters as
r� ¼ ð8=27ÞC0ðT1Þ½cðT2Þ=aðT2Þ � 1�: (10)
The critical stress value r� and corresponding to this stress
temperature T� are the coordinates of the critical point on the
stress–temperature phase diagram.
For the second-order phase transition, the lability tem-
peratures are equal to each other and to the phase transition
temperature. Due to this, the second-order phase transition is
characterized by the anhysteretic continuous change of the
order parameter below the phase transition temperature.
Therefore, the hysteresis of phase transition temperatures is
a distinguishing feature of the first-order phase transitions in
comparison with the second-order ones.
The single crystals of FSMAs usually exhibit a jump-
like transformational behavior: a thermally induced strain
arises in these alloys at certain temperature value (see, e.g.,
Ref. 18). In the case when the phase transition from the ther-
modynamically stable to metastable phase takes place, the
maximal jump of strain value can be observed if the whole
specimen transforms from austenitic to martensitic phase at
T ¼ T2 and from martensitic to austenitic phase at T ¼ T1.
In this case, the hysteresis width is maximal and equals to
DTmax � T1 � T2. The value of DTmax tends to zero on
approaching the critical point of phase diagram.
In many cases, the MT goes gradually, through the
mixed austenitic-martensitic state that is observable in the
temperature interval T2 < T < T1. It was recently argued
that in such cases, the main physical property, which prede-
termines the hysteresis width, is the interrelation between
crystal lattices of martensitic and austenitic phases.19,20 The
ideal compatibility of crystal lattices of parent and product
phases provides the conditions for the observation of low
temperature hysteresis. The hysteresis observed for the for-
ward and reverse MTs going through the mixed two-phase
224903-2 Anna Kosogor J. Appl. Phys. 119, 224903 (2016)
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state is narrower than maximal hysteresis DTmax and, there-
fore, vanishes when the DTmax tends to zero. The suitability
of the given description of hysteresis was already approved
in a very recent experimental work.13
III. THERMODYNAMIC, ELASTIC, ANDMAGNETOELASTIC CHARACTERISTICS OF THEAXIALLY STRESSED FSMA
A. Phase diagram of martensitic transformation
Ni-Mn-Ga alloys are among the most widely studied
FSMAs, so a representative alloy with physical characteristics
close to those of Ni-Mn-Ga alloys is worth consideration.
Although there exists a wide spread of the reported experimen-
tal values of Young’s modulus E (E � 3C0, C0 is a shear modu-
lus)17 from few tens of gigapascals21 to much smaller values,
between 3 GPa and 15 GPa,22–26 generally speaking, these
alloys are very soft near MT, especially, in the carefully grown
single crystalline form. To express this feature, the value of
Young’s modulus equal to EðT1Þ ¼ 3 GPa is used below for
computations. Moreover, typical experimental values of reverse
MT temperature T1ð0Þ ¼ 296 K and tetragonal distortion of
the cubic lattice cðT2Þ=aðT2Þ � 1 ¼ �0:06 are accepted.5
For the chosen values, the energy parameters a4 ¼ 11 GPa,
b4 ¼ 92 GPa and forward MT temperature T2ð0Þ ¼ 278 K
were estimated as explained in Refs. 25 and 27.
Another important measurable characteristic of FSMA
is a magnetoelastic stress.8,17 This stress causes a spontane-
ous and field-induced magnetostrictive deformation of
FSMA. In the twinned martensitic state, the magnetoelastic
stress can trigger a twin structure rearrangement causing a
giant magnetic field-induced strain effect.5,28,29 In particular,
for the twinned Ni-Mn-Ga alloy exhibiting magnetic field-
induced strain studied in Ref. 5, a theoretically estimated
magnetoelastic stress is negative and approximately equals
�5 MPa.8,17
The lability lines T1ðrÞ and T2ðrÞ of martensitic and
austenitic phases at the stress–temperature phase diagram are
determined from Eqs. (8) and (9) and shown in Fig. 1 as a
functions of stress r � rðeff Þ � rðmeÞ < 0, which is induced
by mechanical load. The maximal hysteresis width is
DTmaxðrÞ ¼ T1ðrÞ � T2ðrÞ. The magnetoelastic stress rðmeÞ
is equal to zero in a paramagnetic phase and is approxi-
mately equal to �5 MPa in a ferromagnetic phase.8,17
Strictly speaking, magnetoelastic stress depends on the mag-
netization value, which, in turn, depends on the temperature.
However, the temperature dependence of magnetization is
disregarded here, because for the chosen values of physical
parameters the lability lines (Eqs. (8) and (9)) lie in the MT
temperature range (from 280 to 300 K), while the Curie tem-
peratures of quasistoichiometric Ni-Mn-Ga alloys are much
higher (of about 370 K). For this reason, the rational magnet-
ization change in the MT temperature range is less than or
equal to 0.1. Both T1 and T2 temperatures increase if the
effective stress is negative and decrease otherwise. The
increase/decrease in MT temperatures reflects the martensite
stabilization/destabilization under the axial load.
Figure 1(a) illustrates that both austenitic and marten-
sitic phases are stable in the wide temperature interval (of
about 20 K) if the effective stress equals zero, that is,
r ¼ rðmeÞ ¼ 0. This is the case of MT occurring in an
unstressed paramagnetic crystal. The positive stress destabil-
izes the martensitic phase and therefore retards the forward
(austenitic-martensitic) transformation of the alloy. A desta-
bilizing stress arises, in particular, during the thermomechan-
ical cycling25 and rotation/deflection of magnetic moments
from the equilibrium direction. It should be noted that the
FIG. 1. Stress–temperature phase diagram of the ultra-soft Ni-Mn-Ga shape
memory alloy exhibiting the martensitic transformation in the paramagnetic,
(a), and ferromagnetic, (b), phases. The domain of stability of austenite lies
above the dashed line, while the stability domain of martensitic phase is situ-
ated under the solid line. (c) The experimental13 (dashed lines) and theoreti-
cal (solid lines) phase diagram obtained for ferromagnetic Fe-Pd alloy.
224903-3 Anna Kosogor J. Appl. Phys. 119, 224903 (2016)
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16:14:28
lability line of the paramagnetic austenitic phase is tangential
to the vertical line r ¼ 0 shown in Fig. 1(a) (for more details,
see Ref. 14). It means that the forward temperature-induced
MT cannot be completed and the vertical line r ¼ const > 0
(which is also shown in Fig. 1(a)) does not cross the lability
line of the austenitic phase. Therefore, the volume fraction of
this phase is not equal to zero. It should be emphasized that
this feature of theoretical phase diagram creates favorable
thermodynamic conditions for the “kinetic arrest” of MT
observed in the Ni-Co-Mn-(Ga,Sn,In) alloys,30–32 because
even small local stresses arising during MT can stabilize the
austenitic phase.
The magnetoelastic stress reduces the hysteresis of MT
in Ni-Mn-Ga alloy to the value of 6 K (see Fig. 1(b)). The
hysteresis of MT temperature range becomes equal to zero
when an additional compressive stress r reaches the value of
�12.5 MPa that corresponds to the critical effective stress r�
(Eq. (10)). The physical meaning of this theoretical result is
explained in Section III B. The experimental phase diagram
measured for Fe-Pd alloy13 is given in Fig. 1(c), where Ms is
the forward transformation start temperature and Af is the
reverse transformation finish temperature. Unfortunately, a set
of parameters needed for the quantitative comparison
of theoretical and experimental results is not measured for Fe-
Pd alloy yet. However, a computation of the maximal hystere-
sis width and its comparison with experimental one can be
carried out using reasonable values of theoretical parameters
eM ¼ 3%, rðeff Þ ¼ �15 MPa, and EðT1Þ ¼ 12:2 GPa. (The
theoretical value eM used for computations is close to the
value resulting from experimental strain-temperature loops,
presented in Fig. 2(b).) The parameters were chosen so that
the theoretical critical stress is equal to the experimental one.
The theoretical and experimental dependences of Ms and Af
on the stress value are presented in Fig. 1(c). The figure shows
that the real hysteresis of MT is much lower than the theoreti-
cal one for the small stress values, but the difference between
the theoretical and experimental values of hysteresis
decreases when the absolute stress value increases from zero
to 20 MPa. It should be emphasized that the theoretical critical
temperature T� ¼ 275 K appeared to be rather close to experi-
mental value of 285 K.
B. Martensitic transformation strain
The spontaneous deformation of the crystal lattice (MT
strain) is one of the main characteristics of MT. The theo-
retical temperature dependence of MT strain of axially
stressed Ni-Mn-Ga alloy is shown in Fig. 2(a). This depend-
ence was computed using Eq. (6). The computations show
that the larger the compressive stress is, the smaller the
jumps of MT strain value are in the course of both forward
and reverse MTs. The jumps disappear at the stress value
r� ¼ r� rðmeÞ � �12:5 MPa and continuous anhysteretic
deformation takes place. It means that the first-order phase
transition does not occur if the stress exceeds the critical
value. This statement also follows from the phase diagram
shown in Fig. 1(b): the cooling process at the fixed stress
value r ¼ const (where r < r� � �12:5 MPa) can be pre-
sented in this phase diagram as the vertical line that does
not cross the lability lines. It means that this process does
not result in the phase transition. Instead, a nonlinear con-
tinuous deformation takes place.
Figure 2(a) shows that the application of mechanical
stress decreases temperature hysteresis and after critical
stress r� hysteresis disappears. Moreover, at temperature
T ¼ 290 K, the MT strain computed for the stresses r ¼0 MPa and r ¼ �5 MPa is approximately equal, whereas the
hysteresis width corresponding to r ¼ �5 MPa is smaller by
a factor 0.5. It is also seen that the mechanical stress
increases the transformation temperatures. The similar trans-
formational behavior was observed experimentally in Ref.
13 for the Fe-Pd alloy. The experimental strain-temperature
loops observed for Fe-Pd alloy are shown in Fig. 2(b) to
compare with the theoretical ones calculated for Ni-Mn-Ga
alloy (Fig. 2(a)). Figure 2 shows that the qualitative agree-
ment between the theoretically described and experimentally
observed transformational behavior of axially stressed SMAs
takes place.
The hysteretic phenomena are inherent not only to the
temperature-induced but also to the stress-induced MTs.
However, the anhysteretic stress-induced deformation of
FIG. 2. (a) Hysteresis loops calculated for the forward and reverse MTs in
Ni-Mn-Ga alloy; the hysteresis is absent if the stress exceeds the critical
value. (b) Experimental strain-temperature dependences reported by Xiao
et al.13 for Fe-Pd alloy are shown in comparison with theoretical ones.
224903-4 Anna Kosogor J. Appl. Phys. 119, 224903 (2016)
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FSMA is predicted by the present theory and observed
experimentally at temperatures T > T� for the Ni-Fe(Co)-Ga
alloy (see Ref. 12). The anhysteretic postcritical deformation
is promising for applications because of its giant (>12%)
value.12
The critical stress that provides the experimental obser-
vation of an anhysteretic deformation of an alloy is described
by Eq. (10). According to this equation, a critical stress is
equal to jr�j � 17:5 MPa for the ultra-soft alloy with
C0ðT1Þ ¼ 1 GPa. If the shear modulus C0ðT1Þ exceeds the
value of 20 GPa, which is rather typical for the ferromag-
netic and nonmagnetic SMAs, the critical stress is larger
than 350 MPa. In many cases, the axial stress above 300 MPa
breaks the testing sample. Therefore, the ultra-soft SMAs
deserve a special attention of researchers.
C. Shear elastic modulus of Ni-Mn-Ga single crystal
The shear elastic modulus of the deformable ferromag-
netic crystal is different from that of unstressed paramagnetic
crystal and can be defined as
C0ðT; rÞ ¼ �½@u3ðTÞ=@r��1: (11)
The temperature-dependent lattice distortion is involved in
Eq. (11) through the function u3ðTÞ ¼ 2½cðTÞ=aðTÞ � 1�,which characterizes the tetragonal lattice distortion and pre-
determines the difference in the values of shear modulus of
the austenitic and martensitic phases. Moreover, the values
of lattice parameters and MT strain of the axially stressed
alloy specimen are noticeably different from those observed
at zero stress (Fig. 2(a)). Thus, the shear elastic modulus
depends on the value of mechanical loading.
Figure 3(a) shows the temperature dependences of
Young’s modulus (E � 3C0) of ferromagnetic crystal, which
undergoes the forward and reverse MTs. According to the
assumption formulated previously, the cooled specimen is in
austenitic phase above the temperature T2ðrðmeÞÞ ¼ 291:5 K
and in the martensitic phase below it. In the austenitic phase,
the equality EðTÞ ¼ 9c2ðTÞ occurs.12 The coefficient c2ðTÞof Landau expansion for Gibbs potential (1) vanishes at
T ¼ T2, and the Young’s modulus of austenitic phase
becomes equal to zero at this temperature. The computed
Young’s modulus of the martensitic phase has finite value of
5 GPa at T ¼ T2ðrðmeÞÞ ¼ 292 K. This value is close to the
experimental values of Young’s modulus measured for ferro-
magnetic SMAs at MT temperature.22–26 The heated speci-
men is assumed to be in the martensitic phase at the
temperature below T1ðrðmeÞÞ ¼ 297 K and in the austenitic
phase above it. Therefore, the distance between the minimal
values of Young’s modulus of heated and cooled specimen is
equal to the maximal hysteresis value.
The dependences shown in Fig. 3(a) have unusual fea-
ture: they practically coincide everywhere except for the nar-
row temperature interval DT � 5 K, corresponding to the
temperature hysteresis of MT. This feature was experimen-
tally observed, in particular, for the cubic-rhombohedral
(B2! R) phase transformation of Ti-Ni alloy.33
The influence of axial compressive stress on Young’s
modulus of cooled and heated FSMA is illustrated in Fig.
3(b). It is seen that the application of the compressive stress
increases the value of shear modulus of martensitic phase and
shifts the transformation temperature to a high-temperature
range. Moreover, Figure 3 shows that the rational change of
Young’s modulus under compressive stress increases signifi-
cantly on approach to the MT temperature range: the stress
of �15 MPa results in the change of Young’s modulus
DEðT; rÞ=EðT; 0Þ � 1 at room temperature. Similar behavior
was experimentally observed in Ref. 21 for the Ni-Mn-Ga
alloy under compressive stress. In this work, the rational
change of shear modulus DC0ðrÞ=C0ð0Þ � 0:7 was observed
for the compressive stress of �10 MPa.
D. Magnetostriction of Ni-Mn-Ga alloy
Let the magnetic field be applied in [110]jjz direction to
z-variant of Ni-Mn-Ga martensite with c=a < 1. In this case,
the x- and y-directions are physically equivalent, and there-
fore, rðeff Þ2 ¼ 0. Due to this, Eq. (4) has solution of u2 ¼ 0
and Eqs. (6) and (11) hold.
The magnetoelastic stress value depends on the tempera-
ture as
FIG. 3. (a) Temperature variation of Young’s modulus during heating
(dashed line) and cooling (solid line) of the unloaded ferromagnetic Ni-Mn-
Ga single crystal. (b) Influence of axial load on the temperature variation of
Young’s modulus of a ferromagnetic Ni-Mn-Ga single crystal.
224903-5 Anna Kosogor J. Appl. Phys. 119, 224903 (2016)
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16:14:28
rðmeÞzz ðT;HSÞ ¼ rðmeÞ
3 ðT;HSÞ=2 ¼ �6dM2SðTÞ; (12)
where HS and MS are the saturating magnetic field and the
saturation magnetization, respectively, and d ¼ �23 is a
dimensionless magnetoelastic constant (for more details, see
Ref. 17).
In the case if the alloy specimen is axially stressed by the
axial load, the elastic modulus depends on the stress value r.
The transversal (with respect to the field) magnetostriction of
martensite can be evaluated from an obvious relationship
eðmsÞzz ðT;HS; rÞ ¼ rðmeÞ
zz ðT;HSÞ � rðmeÞzz ðT; 0Þ
h i=EðT; rÞ (13)
received from Eqs. (6), (11), and (12), where EðT; rÞdependences depicted in Fig. 3 can be used for computations.
The inequalities rðmeÞzz ðT; 0Þ < 0, rðmeÞ
zz ðT;HSÞ > 0 hold and
the strain (Eq. (13)) is therefore positive. The plots of satu-
rated magnetoelastic strains (magnetostriction) of FSMA are
shown in Fig. 4 for forward and reverse MTs. The theoretical
curves, presented in Fig. 4, were obtained using the constant
value of saturation magnetization MS ¼ 600 G, which is
close to the value inherent to the Ni-Mn-Ga alloys at room
temperature. The constant magnetization value can be
accepted because the computations were carried out for the
temperatures well below the Curie point of Ni-Mn-Ga,
TC � 375 K.17
Figure 4(a) shows the theoretical temperature dependen-
ces of magnetostriction of the Ni-Mn-Ga single crystal that
undergoes the forward (solid line) and reverse (dashed line)
phase transitions between the cubic phase and single-variant
tetragonal state in the saturating magnetic field. The solid
line shows that the magnetoelastic strain of about 1% as
large can be achieved in the austenitic phase on approach of
the alloy temperature to the forward MT temperature. The
forward MT is accompanied by the abrupt decrease in mag-
netostriction to the value of about 0.2%. This theoretical
result is in qualitative agreement with the experimental data
reported in Ref. 17 for the low-temperature Ni-Mn-Ga as
well as with the data of Ref. 34, where Ni-Mn-Ga with the
martensite start temperature of about 271 K was studied.
In Ref. 34, a pronounced increase in magnetostriction of
the crystal being in cubic phase from the moderate value of
� 0:01% to the large value of 0:1% was observed on
approaching to MT temperature. The computations show
that the magnetostriction of 0.1% corresponds to the rela-
tively large values of shear elastic modulus (�20 GPa)
obtained for the Ni-Mn-Ga alloy specimens in the early
experiments.21 The elevated magnetostriction values shown
in Fig. 4 were computed for the value C0ðT1Þ ¼ 1 GPa, which
is close to the values measured in the ultra-soft alloys.22–26
Figure 4(b) illustrates the reduction and disappearance
of hysteresis of magnetostriction under the applied compres-
sive stress. It is also seen that the stress shifts the temperature
interval where the elevated values of magnetostriction are
observable.
IV. SUMMARY
The low values of shear elastic modulus are inherent to
the single crystalline ferromagnetic shape memory
alloys.12,22–26 The computations carried out for the represen-
tative FSMA showed that the weak axial stress of about few
megapascals drastically reduces the hysteresis width of
temperature-induced MT. The anhysteretic deformational
behavior of FSMA under the stress exceeding the critical
value is described. The critical stress value was expressed
through the shear elastic modulus of austenitic phase, C0, and
lattice constants of the martensitic phase (Eq. (10)). The esti-
mations carried for the representative FSMA showed that the
critical stress is roughly proportional to C0ðT1Þ, where T1 is
the temperature of the reverse MT, and varies from 17.5 MPa
to 350 MPa if the C0ðT1Þ rises from 1 GPa to 20 GPa.
Therefore, SMAs with low values of soft elastic modulus are
the candidates for the observation of large anhysteretic defor-
mations and deserve a special attention as the objects for the
fundamental studies and practical applications.
The recent experimental results obtained in Ref. 13 for
the Fe-Pd alloy were analyzed. A good agreement between
theoretical and experimental dependences of hysteresis width
on the axial stress value was demonstrated.
The hysteresis of temperature dependence of shear mod-
ulus was studied to estimate the temperature dependences of
ordinary axial magnetostriction during the forward and
FIG. 4. (a) Temperature dependences of saturation magnetostriction com-
puted for cooling and heating of Ni-Mn-Ga alloy in the absence of applied
stress. (b) The behavior of magnetostriction under different values of axial
stress in the same alloy.
224903-6 Anna Kosogor J. Appl. Phys. 119, 224903 (2016)
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reverse MTs. A drastic increase in magnetostriction in the
temperature ranges of these MTs was described.
ACKNOWLEDGMENTS
The author is grateful to Victor A. L’vov for his fruitful
discussions. The financial supports from the Ministry of
Education and Science of the Russian Federation in the
framework of Increase Competitiveness Program of NUST
“MISiS” (No. R4-2014-034) and the National Academy of
Sciences of Ukraine (No. 0112U001009) are acknowledged.
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