Acoustoelastic effect


The acoustoelastic effect is how the sound velocities of an elastic material change if subjected to an initial static stress field. This is a non-linear effect of the constitutive relation between mechanical stress and finite strain in a material of continuous mass. In classical linear elasticity theory small deformations of most elastic materials can be described by a linear relation between the applied stress and the resulting strain. This relationship is commonly known as the generalised Hooke's law. The linear elastic theory involves second order elastic constants and yields constant longitudinal and shear sound velocities in an elastic material, not affected by an applied stress. The acoustoelastic effect on the other hand include higher order expansion of the constitutive relation between the applied stress and resulting strain, which yields longitudinal and shear sound velocities dependent of the stress state of the material. In the limit of an unstressed material the sound velocities of the linear elastic theory are reproduced.
The acoustoelastic effect was investigated as early as 1925 by Brillouin. He found that the propagation velocity of acoustic waves would decrease proportional to an applied hydrostatic pressure. However, a consequence of his theory was that sound waves would stop propagating at a sufficiently large pressure. This paradoxical effect was later shown to be caused by the incorrect assumptions that the elastic parameters were not affected by the pressure.
In 1937 Murnaghan presented a mathematical theory extending the linear elastic theory to also include finite deformation in elastic isotropic materials. This theory included three third-order elastic constants,, and. In 1953 Huges and Kelly used the theory of Murnaghan in their experimental work to establish numerical values for higher order elastic constants for several elastic materials including Polystyrene, Armco iron, and Pyrex, subjected to hydrostatic pressure and uniaxial compression.

Non-linear elastic theory for hyperelastic materials

The acoustoelastic effect is an effect of finite deformation of non-linear elastic materials. A modern comprehensive account of this can be found in. This book treats the application of the non-linear elasticity theory and the analysis of the mechanical properties of solid materials capable of large elastic deformations. The special case of the acoustoelastic theory for a compressible isotropic hyperelastic material, like polycrystalline steel, is reproduced and shown in this text from the non-linear elasticity theory as presented by Ogden.

Constitutive relation – hyperelastic materials (Stress-strain relation)

A hyperelastic material is a special case of a Cauchy elastic material in which the stress at any point is objective and determined only by the current state of deformation with respect to an arbitrary reference configuration. However, the work done by the stresses may depend on the path the deformation takes. Therefore, a Cauchy elastic material has a non-conservative structure, and the stress cannot be derived from a scalar elastic potential function. The special case of Cauchy elastic materials where the work done by the stresses is independent of the path of deformation is referred to as a Green elastic or hyperelastic material. Such materials are conservative and the stresses in the material can be derived by a scalar elastic potential, more commonly known as the Strain energy density function.
The constitutive relation between the stress and strain can be expressed in different forms based on the chosen stress and strain forms. Selecting the 1st Piola-Kirchhoff stress tensor , the constitutive equation for a compressible hyper elastic material can be expressed in terms of the Lagrangian Green strain as:
where is the deformation gradient tensor, and where the second expression uses the Einstein summation convention for index notation of tensors. is the strain energy density function for a hyperelastic material and have been defined per unit volume rather than per unit mass since this avoids the need of multiplying the right hand side with the mass density of the reference configuration.
Assuming that the scalar strain energy density function can be approximated by a Taylor series expansion in the current strain, it can be expressed as:
Imposing the restrictions that the strain energy function should be zero and have a minimum when the material is in the un-deformed state it is clear that there are no constant or linear term in the strain energy function, and thus:
where is a fourth-order tensor of second-order elastic moduli, while is a sixth-order tensor of third-order elastic moduli.
The symmetry of together with the scalar strain energy density function implies that the second order moduli have the following symmetry:
which reduce the number of independent elastic constants from 81 to 36. In addition the power expansion implies that the second order moduli also have the major symmetry
which further reduce the number of independent elastic constants to 21. The same arguments can be used for the third order elastic moduli. These symmetries also allows the elastic moduli to be expressed by the Voigt notation.
The deformation gradient tensor can be expressed in component form as
where is the displacement of a material point from coordinate in the reference configuration to coordinate in the deformed configuration. Including the power expansion of strain energy function in the constitutive relation and replacing the Lagrangian strain tensor with the expansion given on the finite strain tensor page yields the constitutive equation
where
and higher order terms have been neglected
.
For referenceM by neglecting higher order terms in this expression reduce to
which is a version of the generalised Hooke's law where is a measure of stress while is a measure of strain, and is the linear relation between them.

Sound velocity

Assuming that a small dynamic deformation disturb an already statically stressed material the acoustoelastic effect can be regarded as the effect on a small deformation superposed on a larger finite deformation. Let us define three states of a given material point. In the reference state the point is defined by the coordinate vector while the same point has the coordinate vector in the static initially stressed state. Finally, assume that the material point under a small dynamic disturbance have the coordinate vector. The total displacement of the material points can then be described by the displacement vectors
where
describes the static initial displacement due to the applied pre-stress, and the displacement due to the acoustic disturbance, respectively.
Cauchy's first law of motion for the additional Eulerian disturbance can then be derived in terms of the intermediate Lagrangian deformation assuming that the small-on-large assumption
holds.
Using the Lagrangian form of Cauchy's first law of motion, where the effect of a constant body force has been neglected, yields
The right hand side of the law of motion can be expressed as
under the assumption that both the unstressed state and the initial deformation state are static and thus.
For the left hand side the spatial Lagrangian partial derivatives with respect to can be expanded in the Eulerian by using the chain rule and changing the variables through the relation between the displacement vectors as
where the short form has been used. Thus
Assuming further that the static initial deformation is in equilibrium means that, and the law of motion can in combination with the constitutive equation given above be reduced to a linear relation between the static initial deformation and the additional dynamic disturbance as
where
This expression is recognised as the linear wave equation. Considering a plane wave of the form
where is a Lagrangian unit vector in the direction of propagation, is a unit vector referred to as the polarization vector, is the phase wave speed, and is a twice continuously differentiable function. Inserting this plane wave in to the linear wave equation derived above yields
where is introduced as the acoustic tensor, and depends on as
This expression is called the propagation condition and determines for a given propagation direction the velocity and polarization of possible waves corresponding to plane waves. The wave velocities can be determined by the characteristic equation
where is the determinant and is the identity matrix.
For a hyperelastic material is symmetric, and the eigenvalues are thus real. For the wave velocities to also be real the eigenvalues need to be positive. If this is the case, three mutually orthogonal real plane waves exist for the given propagation direction. From the two expressions of the acoustic tensor it is clear that
and the inequality for all non-zero vectors and guarantee that the velocity of homogeneous plane waves are real. The polarization corresponds to a longitudinal wave where the particle motion is parallel to the propagation direction. The two polarizations where corresponds to transverse waves where the particle motion is orthogonal to the propagation direction.

Isotropic materials

Elastic moduli for isotropic materials

For a second order isotropic tensor like the Lagrangian strain tensor have the invariants where is the trace operator, and. The strain energy function of an isotropic material can thus be expressed by, or a superposition there of, which can be rewritten as
where are constants. The constants and are the second order elastic moduli better known as the Lamé parameters, while and are the third order elastic moduli introduced by, which are alternative but equivalent to and introduced by Murnaghan.
Combining this with the general expression for the strain energy function it is clear that
where. Historically different selection of these third order elastic constants have been used, and some of the variations is shown in Table 1.

Example values for steel

Table 2 and 3 present the second and third order elastic constants for some steel types presented in literature

Acoustoelasticity for uniaxial tension of isotropic hyperelastic materials

A cuboidal sample of a compressible solid in an unstressed reference configuration can be expressed by the Cartesian coordinates, where the geometry is aligned with the Lagrangian coordinate system, and is the length of the sides of the cuboid in the reference configuration. Subjecting the cuboid to a uniaxial tension in the -direction so that it deforms with a pure homogeneous strain such that the coordinates of the material points in the deformed configuration can be expressed by, which gives the
elongations
in the -direction. Here signifies the current length of the cuboid side and where the ratio between the length of the sides in the current and reference configuration are denoted by
called the principal stretches. For an isotropic material this corresponds to a deformation without any rotation. This can be described through spectral representation by the principal stretches as eigenvalues, or equivalently by the elongations.
For a uniaxial tension in the -direction the lateral elongations and are limited to the range. For isotropic symmetry the lateral elongations must also be equal. The range corresponds to the range from total lateral contraction, and to no change in the lateral dimensions. It is noted that theoretically the range could be expanded to values large than 0 corresponding to an increase in lateral dimensions as a result of increase in axial dimension. However, very few materials exhibit this property.

Expansion of sound velocities

If the strong ellipticity condition holds, three orthogonally polarization directions, one selection of orthonormal polarizations may be
which gives the three sound velocities
where the first index of the sound velocities indicate the propagation direction.
Expanding the relevant coefficients of the acoustic tensor, and substituting the second- and third-order elastic moduli and with their isotropic equivalents, and respectively, leads to the sound velocities expressed as
where
are the acoustoelastic coefficients related to effects from third order elastic constants.

Measurement methods

To be able to measure the sound velocity, and more specifically the change in sound velocity, in a material subjected to some stress state, one can measure the velocity of an acoustic signal propagating through the material in question. There are several methods to do this but all of them use one of two physical relations of the sound velocity. The first relation is related to the time it takes a signal to propagate from one point to another. This is often referred to as "Time-of-flight" measurements, and use the relation
where is the distance the signal travels and is the time it takes to travel this distance. The second relation is related to the inverse of the time, the frequency, of the signal. The relation here is
where is the frequency of the signal and is the wave length. The measurements using the frequency as measurand use the phenomenon of acoustic resonance where number of wave lengths match the length over which the signal resonate. Both these methods are dependent on the distance over which it measure, either directly as in the Time-of-flight, or indirectly through the matching number of wavelengths over the physical extent of the specimen which resonate.

Example of ultrasonic testing techniques

In general there are two ways to set up a transducer system to measure the sound velocity in a solid. One is a setup with two or more transducers where one is acting as a transmitter, while the other is acting as a receiver. The sound velocity measurement can then be done by measuring the time between a signal is generated at the transmitter and when it is recorded at the receiver while assuming to know the distance the acoustic signal have traveled between the transducers, or conversely to measure the resonance frequency knowing the thickness over which the wave resonate. The other type of setup is often called a pulse-echo system. Here one transducer is placed in the vicinity of the specimen acting both as transmitter and receiver. This requires a reflective interface where the generated signal can be reflected back toward the transducer which then act as a receiver recording the reflected signal. See ultrasonic testing for some measurement systems.

Longitudinal and polarized shear waves

As explained above, a set of three orthonormal polarizations of the particle motion exist for a given propagation direction in a solid. For measurement setups where the transducers can be fixated directly to the sample under investigation it is possible to create these three polarizations by applying different types of transducers exciting the desired polarization. Thus it is possible to measure the sound velocity of waves with all three polarizations through either time dependent or frequency dependent measurement setups depending on the selection of transducer types. However, if the transducer can not be fixated to the test specimen a coupling medium is needed to transmit the acoustic energy from the transducer to the specimen. Water or gels are often used as this coupling medium. For measurement of the longitudinal sound velocity this is sufficient, however fluids do not carry shear waves, and thus to be able to generate and measure the velocity of shear waves in the test specimen the incident longitudinal wave must interact at an oblique angle at the fluid/solid surface to generate shear waves through mode conversion. Such shear waves are then converted back to longitudinal waves at the solid/fluid surface propagating back through the fluid to the recording transducer enabling the measurement of shear wave velocities as well through a coupling medium.

Applications

Engineering material – stress estimation

As the industry strives to reduce maintenance and repair costs, non-destructive testing of structures becomes increasingly valued both in production control and as a means to measure the utilization and condition of key infrastructure. There are several measurement techniques to measure stress in a material. However, techniques using optical measurements, magnetic measurements, X-ray diffraction, and neutron diffraction are all limited to measuring surface or near surface stress or strains. Acoustic waves propagate with ease through materials and provide thus a means to probe the interior of structures, where the stress and strain level is important for the overall structural integrity.
Since the sound velocity of such non-linear elastic materials have a stress dependency, one application of the acoustoelastic effect may be measurement of the stress state in the interior of a loaded material utilizing different acoustic probes to measure the change in sound velocities.

Granular and porous materials – geophysics

study the propagation of elastic waves through the Earth and is used in e.g. earthquake studies and in mapping the Earth's interior. The interior of the Earth is subjected to different pressures, and thus the acoustic signals may pass through media in different stress states. The acoustoelastic theory may thus be of practical interest where nonlinear wave behaviour may be used to estimate geophysical properties.

Soft tissue – medical ultrasonics

Other applications may be in medical sonography and elastography measuring the stress or pressure level in relevant elastic tissue types
, enhancing non-invasive diagnostics.