
| *Corresponding Author Contact: Jet Propulsion Laboratory (JPL), Caltech, Pasadena, CA, USA 91109; yosi@jpl.nasa.gov; http://ndeaa.jpl.nasa.gov |
Full-Text - AbstractRecently, the authors modified their experimental setup to allow measuring dispersion curves at a significantly higher speed than ever recorded. A set of 20 angles of incidence along a single polar angle of a composite laminate are acquired in about 45 second. The reflection spectra are acquired in real time while filtering the high frequency noise allowing to obtain reliable data at ranges of amplitudes that are much lower that were used in prior studies. This method makes the LLW a practical quantitative tool for both inversion of the elastic properties and flaw characterization. The emphasis of the current study is on the detection and characterization of flaws. The composite is modeled as transversely isotropic and dissipative medium and the effect of flaws is analyzed and compared to the experimental data using a C-scan mounted LLW scanner.
ACKNOWLEDGMENT
The reported efforts was sponsored by the U.S. Air Force Office of Scientific Research, Air Force Materiel Command, USAF, under grant number F49620-95-1-0518.
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Abstract Source:
Book of Abstracts, 7th European Conference on Non-Destructive Testing, 26-29 May 1998, ISBN: 87-986898-0-00
Full-Text Source:
Proceedings of the 7th European Conference on Non-Destructive Testing, 26-29 May 1998, ISBN:
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