DocumentCode :
296834
Title :
A robust technique for estimating visco-elastic stiffnesses of plates using air-coupled ultrasound
Author :
Safaeinili, A. ; Lobkis, O.I. ; Chimenti, D.E.
Author_Institution :
Center for Nondestructive Evaluation, Iowa State Univ., Ames, IA, USA
Volume :
1
fYear :
1995
fDate :
7-10 Nov 1995
Firstpage :
771
Abstract :
A robust technique for estimating visco-elastic stiffnesses of composite plates is presented. Generally, material characterization techniques are based on simplified models which result in inaccurate inversions. The estimation technique presented in this paper is highly accurate since it utilizes a 3-D beam model which accounts fully for diffraction effects and other geometrical and experimental parameters. Furthermore, the air-coupled nature of the experiment enhances the estimation accuracy since it minimizes the couplant loading effects. A significant feature of this technique is its high sensitivity to shear stiffness parameters which are generally difficult to obtain. This technique has been successfully used to obtain stiffness parameters for both isotropic and anisotropic plates with single or multilayer structures
Keywords :
elastic moduli measurement; surface acoustic waves; ultrasonic diffraction; ultrasonic materials testing; viscoelasticity; 3-D beam model; air-coupled ultrasound; anisotropic plates; composite plates; couplant loading effects; diffraction effects; estimation accuracy; estimation technique; geometrical parameters; isotropic plates; multilayer structures; robust technique; shear stiffness parameters; single layer structures; visco-elastic stiffnesses; Acoustic transducers; Composite materials; Geometry; Material properties; Robustness; Solid modeling; Ultrasonic imaging; Ultrasonic transducers; Ultrasonic variables measurement; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Ultrasonics Symposium, 1995. Proceedings., 1995 IEEE
Conference_Location :
Seattle, WA
ISSN :
1051-0117
Print_ISBN :
0-7803-2940-6
Type :
conf
DOI :
10.1109/ULTSYM.1995.495680
Filename :
495680
Link To Document :
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