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Acoustic Emission Monitoring of CFRP Laminated Composites ...

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26 Chapter 3. <strong>Acoustic</strong> <strong>Emission</strong><br />

ized (surface SV-waves) and Love waves are horizontally polarized (surface<br />

SH-waves). Both are dispersive and the amplitudes decreases exponentially<br />

with depth. Flexural waves, or Lamb waves, are a special class <strong>of</strong><br />

waves which occur in plates which are bounded by two surfaces, e.g. laminated<br />

composites. There are three fundamental classes <strong>of</strong> Lamb waves,<br />

analogous to the body waves: LP, LSH, and LSV. 123<br />

Two modes <strong>of</strong> Lamb<br />

waves are observed in thin plates: extensional (symmetric) and exural<br />

(antisymmetric) modes. The largest component <strong>of</strong> the extensional mode<br />

lies in the plane <strong>of</strong> the plate, while the largest exural mode component is<br />

out <strong>of</strong> the plane. 124<br />

The wave velocity in isotropic and homogeneous materials depends on<br />

the density and stiness <strong>of</strong> the material. Fiber-reinforced composites are<br />

anisotropic and inhomogeneous; hence, the wave velocity is anisotropic.<br />

Furthermore, the wave velocity is a function <strong>of</strong> frequency, 123<br />

i.e. high and<br />

low frequency waves will separate as they propagate. This separation is<br />

referred to as dispersion and results in an amplitude decrease. A parameter<br />

which describes the resistance <strong>of</strong> a material to transfer waves is the<br />

acoustic impedance. This parameter is analogous to electrical impedance.<br />

The acoustic impedance depends both on the wave type and the frequency.<br />

It is dened as the product <strong>of</strong> the material density with the velocity <strong>of</strong> the<br />

wave type. When the waves come across inhomogeneities such as defects,<br />

interfaces between the constituent materials <strong>of</strong> the composite, and the surface<br />

<strong>of</strong> the composite, they will reect and refract. The actual response<br />

depends on the acoustic impedance <strong>of</strong> the two adjacent materials and the<br />

angle <strong>of</strong> incidence between the wave and reecting boundary. Assuming<br />

that the wave's energy is conserved, the energy per unit area <strong>of</strong> the wave<br />

decreases as the surface area <strong>of</strong> the wave increases. Hence, the rate <strong>of</strong> decrease<br />

depends on how the wave propagates, e.g. as plane-, spherical- or<br />

cylindrical waves. The wave's energy, however, is not conserved. Due to<br />

internal friction, part <strong>of</strong> the energy is converted into heat. Consequently,<br />

when a stress wave nally arrives at the transducer its waveform parameters<br />

will have changed. For these reasons, the analysis and interpretation<br />

<strong>of</strong> AE signals is a complex subject.

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