| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 9640871 | Journal of Sound and Vibration | 2005 | 21 Pages |
Abstract
The procedure is demonstrated with a finite element model of a plate, and experiments on composite plates with deliberately induced multiple delaminations. Finally, the method is demonstrated on data taken from a large composite hull structure. In all cases the procedure successfully located the damaged regions.
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Authors
M.K. Yoon, D. Heider, J.W. Jr., C.P. Ratcliffe, R.M. Crane,