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Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow

✍ Scribed by Guoyong Zheng

Publisher
The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences
Year
2010
Tongue
English
Weight
513 KB
Volume
26
Category
Article
ISSN
0567-7718

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πŸ“œ SIMILAR VOLUMES

TRANSONIC AND LOW-SUPERSONIC AEROELASTIC
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✍ DONG-HYUN KIM; IN LEE πŸ“‚ Article πŸ“… 2000 πŸ› Elsevier Science 🌐 English βš– 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

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✍ A.P. LEWIS πŸ“‚ Article πŸ“… 2002 πŸ› Elsevier Science 🌐 English βš– 475 KB

It is well known that the presence of non-linearities may signi"cantly a!ect the aeroelastic response of an aerospace vehicle structure. In this paper, the aeroelastic behaviour at high Mach numbers of an all-moving control surface with a non-linearity in the root support is investigated. Very often