2006
DOI: 10.4028/www.scientific.net/amr.13-14.325
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Acoustic Emission in Wide Composite Specimens

Abstract: Acoustic emission (AE) is an attractive technique for the structural health monitoring (SHM) of aerospace systems. To reach its full potential in this role a quantitative approach must be adopted to study damage mechanisms in composite materials. In this paper, some of the practical issues regarding acoustic emission testing in composites are addressed. A model describing Lamb wave propagation through plates is described and used to make phase velocity and attenuation measurements in both aluminium and carbon … Show more

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Cited by 20 publications
(6 citation statements)
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“…1 Generally, the generation, expansion, and accumulation of cracks induce internal, macroscopic cracks in the material, which further affect its service performance and lifetime and eventually lead to catastrophic material failure. Conventional methods of crack location and diagnosis have been developed including optical coherence tomography, 2 microscopy, 3 acoustic emissions, 4 and infrared thermography. 5 Especially, Sottos and co-workers 6 introduced a capsule-based approach for autonomous damage indication in polymers and polymer composites.…”
Section: Introductionmentioning
confidence: 99%
“…1 Generally, the generation, expansion, and accumulation of cracks induce internal, macroscopic cracks in the material, which further affect its service performance and lifetime and eventually lead to catastrophic material failure. Conventional methods of crack location and diagnosis have been developed including optical coherence tomography, 2 microscopy, 3 acoustic emissions, 4 and infrared thermography. 5 Especially, Sottos and co-workers 6 introduced a capsule-based approach for autonomous damage indication in polymers and polymer composites.…”
Section: Introductionmentioning
confidence: 99%
“…The frequencies of these sidebands are equal to (1) where f Sn is the frequency of the n-th (n =1, 2, 3, …, n ) sideband, f H is the frequency of acoustic wave and f L is the frequency of modal excitation. The intensity of modulation can be described by the R parameter, estimated from the relationship between amplitudes of two major sidebands and the high-frequency component, expressed as (2) where A 0 is the spectral amplitude of the carrier acoustical frequency, A 1 and A 2 are the spectral amplitudes of the first pair of sidebands. It is important to mention that often non-damage structures also exhibit small modulation sidebands due to intrinsic nonlinearities (e.g.…”
Section: Nonlinear Acousticsmentioning
confidence: 99%
“…Different faults will generate independent excitations, and the AE measurements obtained will represent a mixture of these excitations sources. 27,28 Segments of raw AE signals in the time domain obtained from the test rig are shown in Fig. 6, which are representative of the signals obtained during the fatigue testing of wind turbine blade samples.…”
Section: A E S I G N a L P R O C E S S I N G R E S U L T Smentioning
confidence: 99%