Underwing Missile Aerodynamic Effects on Flight-Measured Limit-Cycle Oscillations
Author:
Affiliation:
1. Carriage Mechanics Division, 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/10.2514/1.C032216
Reference8 articles.
1. In-Flight Wing Deformation Characteristics During Limit Cycle Oscillations
2. Influence of External Store Aerodynamics on Flutter/LCO of a Fighter Aircraft
3. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
4. Limit Cycle Oscillation Characteristics of Fighter Aircraft
5. Role of shock dynamics in transonic flutter
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2. Aeroelastic Energy Analysis Using Distributed Aerodynamic Work Visualization;AIAA Journal;2017-06
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