Computational Study of Transonic Limit Cycle Oscillation Phenomenon on F-16 Fighter Aircraft
Author:
Affiliation:
1. Israel Air Force, 6473428 Tel Aviv, Israel
2. Technion—Israel Institute of Technology, 32000 Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033918
Reference34 articles.
1. Limit Cycle Oscillation Characteristics of Fighter Aircraft
2. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
3. In-Flight Wing Deformation Characteristics During Limit Cycle Oscillations
4. EdwardsJ. W.SchusterD. M.SpainC. V.KellerD. F.MosesR. W. “Mavric Flutter Model Transonic Limit Cycle Oscillation Test,” NASA TM-2001-210877, May 2001.
5. Nonlinear effects in transonic flutter with emphasis on manifestations of limit cycle oscillations
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