Guided waves in anisotropic and quasi-isotropic aerospace composites: Three-dimensional simulation and experiment

被引:103
作者
Leckey, Cara A. C. [1 ]
Rogge, Matthew D. [1 ]
Parker, F. Raymond [1 ]
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
关键词
Guided wave; Finite integration; Simulation; Composite; Delamination; FINITE INTEGRATION TECHNIQUE; FIBER-REINFORCED POLYMER; IMPACT DAMAGE; PREDICTION; SCATTERING;
D O I
10.1016/j.ultras.2013.05.007
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Three-dimensional (3D) elastic wave simulations can be used to investigate and optimize nondestructive evaluation (NDE) and structural health monitoring (SHM) ultrasonic damage detection techniques for aerospace materials. 3D anisotropic elastodynamic finite integration technique (EFIT) has been implemented for ultrasonic waves in carbon fiber reinforced polymer (CFRP) composite laminates. This paper describes 3D EFIT simulations of guided wave propagation in undamaged and damaged anisotropic and quasi-isotropic composite plates. Comparisons are made between simulations of guided waves in undamaged anisotropic composite plates and both experimental laser Doppler vibrometer (LDV) wavefield data and dispersion curves. Time domain and wavenumber domain comparisons are described. Wave interaction with complex geometry delamination damage is then simulated to investigate how simulation tools incorporating realistic damage geometries can aid in the understanding of wave interaction with CFRP damage. In order to move beyond simplistic assumptions of damage geometry, volumetric delamination data acquired via X-ray microfocus computed tomography is directly incorporated into the simulation. Simulated guided wave interaction with the complex geometry delamination is compared to experimental LDV time domain data and 3D wave interaction with the volumetric damage is discussed. Published by Elsevier B.V.
引用
收藏
页码:385 / 394
页数:10
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