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Finite element supersonic flutter analysis of skewed and cracked composite panels

โœ Scribed by R.M.V. Pidaparti; C.C. Chang


Publisher
Elsevier Science
Year
1998
Tongue
English
Weight
349 KB
Volume
69
Category
Article
ISSN
0045-7949

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FINITE-ELEMENT ANALYSIS OF THE FLUTTERIN
โœ G. SURACE; R. UDRESCU ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 417 KB

In this article the classical analysis of the static pressure e!ect on #uttering panels is extended to cases of pulse and step excitations. A high order "nite-element methodology is applied within the non-linear elastic, linear aerodynamic theories and a dynamic analysis is performed on a reference