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Aeroelastic analysis of a flexible control surface with structural nonlinearity

โœ Scribed by Lee, In; Kim, Seung-Ho

Book ID
121334794
Publisher
American Institute of Aeronautics and Astronautics
Year
1995
Tongue
English
Weight
784 KB
Volume
32
Category
Article
ISSN
0021-8669

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AEROELASTIC ANALYSIS OF A FLEXIBLE AIRFO
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โœ S.-H. Kim; I. Lee ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 761 KB

A two-dimensional flexible airfoil with a freeplay non-linearity in pitch has been analyzed in the subsonic flow range. Structurally, the airfoil is modelled as finite beam elements and two spring elemens in pitch and plunge. A doublet lattice method is used for the two-dimensional unsteady aerodyna