A new approach to computational aeroelasticity
Author:
Affiliation:
1. California, University, Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-939
Reference17 articles.
1. Time-marching transonic flutter solutions including angle-of-attack effects
2. Application of Transonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils
3. Bendiksen. 0.0.and Kousen, K. A. "Transonic Flutter Analysis Using theEuler Equations,"AIAA Paper 87-0911-CP,April 1987.
4. Nonlinear aspects of the transonic aeroelastic stability problem
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