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Symmetrical Facing Wrinkling of Composite Sandwich Panels

โœ Scribed by Lopatin, A.V.; Morozov, E.V.


Book ID
121836601
Publisher
SAGE Publications
Year
2008
Tongue
English
Weight
386 KB
Volume
10
Category
Article
ISSN
1099-6362

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๐Ÿ“œ SIMILAR VOLUMES


MODAL DENSITY OF COMPOSITE HONEYCOMB SAN
โœ K. Renji; P.S. Nair; S. Narayanan ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 326 KB

Honeycomb sandwich panels with composite face sheets are widely used in spacecraft applications. It is necessary to obtain the modal density of such panels to study their behaviour under acoustic excitation. The governing differential equation, with consideration of the shear flexibility of the core