A technique for the prediction of airfoil flutter characteristics inseparated flow
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
2. Georgia Institute of Technology, Atlanta
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-910
Reference26 articles.
1. Computation of Unsteady Transonic Flows by the Indicial Method
2. Flutter analysis of a NACA 64A006 airfoil in small disturbance transonic flow
Cited by 3 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
1. Effects of structural nonlinearity in the bifurcation analysis of transonic airfoil flutter;Fluid Dynamics Conference;1996-06-17
2. Nonlinear analysis of airfoil flutter at transonic speeds;13th Applied Aerodynamics Conference;1995-06-19
3. Experimental investigation of the flowfield of an oscillating airfoil;10th Applied Aerodynamics Conference;1992-06-22
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