Time-marching transonic flutter solutions including angle-of-attack effects
Author:
Affiliation:
1. NASA, Langley Research Center, Loads and Aeroelasticity Div., Hampton, VA
2. NASA, Langley Research Center; Kentron International, Inc., Hampton,VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-685
Reference35 articles.
1. 3izzetta,D. P."Time-Dependent Response of a Two-Dimensional Airfoil i n Transonic Flow," AIAA Journal, vol.17, no.1, January 1979.
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