Aeroelastic Instability of Cantilever Wing with Added Engine Mass and Thrust Loads Under the Gust Envelope
Author:
Publisher
Springer Science and Business Media LLC
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering,Ocean Engineering,Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.1007/s40032-018-0486-y.pdf
Reference36 articles.
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3. M.D. Conner, D.M. Tang, E.H. Dowell, I.N. Virgin, Nonlinear behavior of a typical airfoil section with control surface freeplay: a numerical and experimental study. J. Fluids Struct. 11, 89–109 (1997)
4. D. Tang, E.H. Dowell, L.N. Virgin, Limit cycle behavior of an airfoil with a control surface. J. Fluids Struct. 12, 839–858 (1998)
5. A. Abdelkefi, R. Vasconcellos, A.H. Nayfeh, M.R. Hajj, An analytical and experimental investigation into limit cycle-oscillations of an aeroelastic system. Nonlinear Dyn. 71, 159–173 (2013)
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