Virtual Aeroelastic Flight Testing for the F-16 Fighter with Stores
Author:
Affiliation:
1. Duke University
2. U.S. Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1640
Reference17 articles.
1. Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique
2. Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations
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