Limit Cycle Oscillation Characteristics of Fighter Aircraft
Author:
Affiliation:
1. U.S. Naval Air Warfare Center, Patuxent River, Patuxent River, Maryland 20670-5304
2. U.S. Air Force SEEK EAGLE Office, Eglin Air Force Base, Florida 32542-6865
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2690
Reference5 articles.
1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
2. 4Airplane Strength and Rigidity-Vibration, Flutter, and Divergence, MIL-SPEC MIL-A-8870B, 20 May 1987, p. 3.
3. F-16 flutter testing at Eglin Air Force Base
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