๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

LOSS FACTORS OF COMPOSITE HONEYCOMB SANDWICH PANELS

โœ Scribed by K. RENJI; S. SHANKAR NARAYAN


Publisher
Elsevier Science
Year
2002
Tongue
English
Weight
266 KB
Volume
250
Category
Article
ISSN
0022-460X

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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

EXPERIMENTAL MODAL DENSITIES OF HONEYCOM
โœ K. RENJI ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 178 KB

The model density of a structure can be experimentally determined from the real part of its driving point admittance. Due to the impedance of the impedance head and the attachment elements, the measured admittance values can be di!erent from the actual driving point admittance, especially at higher