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A study on composite honeycomb sandwich panel structure

✍ Scribed by Meifeng He; Wenbin Hu


Book ID
108200756
Publisher
Elsevier Science
Year
2008
Weight
140 KB
Volume
29
Category
Article
ISSN
0261-3069

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πŸ“œ SIMILAR VOLUMES


MODAL DENSITY OF COMPOSITE HONEYCOMB SAN
✍ K. Renji; P.S. Nair; S. Narayanan πŸ“‚ Article πŸ“… 1996 πŸ› Elsevier Science 🌐 English βš– 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