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Finite Element Method Applied to Supersonic Flutter of Circular Cylindrical Shells

โœ Scribed by Sabri, Farhad; Lakis, Aouni A.


Book ID
120557827
Publisher
American Institute of Aeronautics and Astronautics
Year
2010
Tongue
English
Weight
537 KB
Volume
48
Category
Article
ISSN
0001-1452

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Field-Consistent Element Applied to Flut
โœ M. Ganapathi; T.K. Varadan; J. Jijen ๐Ÿ“‚ Article ๐Ÿ“… 1994 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 455 KB

Supersonic flutter analysis of laminated composite circular cylindrical shells is investigated by using an axisymmetric shell finite element based on the field-consistency approach. The formulation includes transverse shear deformation and in-plane and rotary inertia effects. The aerodynamic force i