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Bifurcation analysis of a two-degree-of-freedom aeroelastic system with freeplay structural nonlinearity by a perturbation-incremental method

โœ Scribed by K.W. Chung; C.L. Chan; B.H.K. Lee


Publisher
Elsevier Science
Year
2007
Tongue
English
Weight
414 KB
Volume
299
Category
Article
ISSN
0022-460X

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๐Ÿ“œ SIMILAR VOLUMES


TRANSONIC AND LOW-SUPERSONIC AEROELASTIC
โœ DONG-HYUN KIM; IN LEE ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 487 KB

A two-degree-of-freedom airfoil with a freeplay non-linearity in the pitch and plunge directions has been analyzed in the transonic and low-supersonic #ow region, where aerodynamic non-linearities also exist. The primary purpose of this study is to show aeroelastic characteristics due to freeplay st