MODAL DENSITY OF COMPOSITE HONEYCOMB SAN
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K. Renji; P.S. Nair; S. Narayanan
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Article
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1996
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Elsevier Science
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English
β 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