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
ANALYSIS AND COMPUTATION OF NONLINEAR DYNAMIC RESPONSE OF A TWO-DEGREE-OF-FREEDOM SYSTEM AND ITS APPLICATION IN AEROELASTICITY
β Scribed by B.H.K. Lee; L. Gong; Y.S. Wong
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 478 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0889-9746
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