Author:
Sazesh Saeid,Shams Shahrokh
Funder
Iran National Science Foundation
INSF
University of Tehran
Reference29 articles.
1. Asjes, D., Diwadkar, A., Vaidya, U., Kelkar, A., Vogel, J.M., Chaussee, D., 2014. Modeling and analysis of rotational freeplay nonlinearity of a 2D airfoil. In: 2014 American Control Conference, pp. 1162-1167
2. Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface;Bae;J. Fluids Struct.,2004
3. Ative wing flutter suppression using a trailing edge flap;Borglund;J. Fluids Struct.,2002
4. PrandtlPlane Joined Wing: Body freedom flutter, limit cycle oscillation and freeplay studies;Cavallaro;J. Fluids Struct.,2015
5. Nonlinear aeroelastic analysis of an airfoil-store system with a freeplay by precise integration method;Chen;J. Fluids Struct.,2014
Cited by
14 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献