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Flutter of dynamically nonuniform airfoil cascades in potential flow

โœ Scribed by A. N. Fedosova

Book ID
112555078
Publisher
Springer
Year
1974
Tongue
English
Weight
303 KB
Volume
6
Category
Article
ISSN
0039-2316

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The limit cycle #utter of a two-dimensional wing with non-linear pitching sti!ness is investigated. For modelling the aerodynamic forces of the wing steady linear and non-linear models as well as an unsteady model were used. The #utter speed was calculated using the harmonic balance method and by pr