Aerodynamic lag functions, divergence, and the British flutter method
Author:
Affiliation:
1. The MacNeal-Schwendler Corporation, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44772
Reference18 articles.
1. A strip method for prediction of damping in subsonic wind tunnel andflight flutter tests.
2. A MORE REALISTIC METHOD FOR ROUTINE FLUTTER CALCULATIONS
3. Subsonic Transient Lifting Surface Aerodynamics
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