LIMIT CYCLE FLUTTER OF AIRFOILS IN STEAD
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P. SHAHRZAD; M. MAHZOON
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Article
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2002
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Elsevier Science
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English
β 626 KB
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