Identification Approach to Estimate Buckling Load of Damaged Composite Plates

The application of an indirect approach for prediction of buckling loads of laminated composite plates with flaws or damage, based on the indentification of the flexibilty influence function of the damaged plate through experimentally measured modal vibration characteristics, is presented.

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Veröffentlicht in:AIAA journal 1998-08, Vol.36 (8), p.1479-1485
Hauptverfasser: Salunkhe, Anil L, Mujumdar, Prasanna M
Format: Artikel
Sprache:eng
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Zusammenfassung:The application of an indirect approach for prediction of buckling loads of laminated composite plates with flaws or damage, based on the indentification of the flexibilty influence function of the damaged plate through experimentally measured modal vibration characteristics, is presented.
ISSN:0001-1452
1533-385X
DOI:10.2514/2.540