Modeling Delta Wing Limit-Cycle Oscillations Using a High-Fidelity Structural Model
Author:
Affiliation:
1. Computational Sciences Branch, Wright–Patterson AFB, Ohio 4533-7913
2. Duke University, Durham, North Carolina 27708
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11325
Reference16 articles.
1. Limit Cycle Oscillations of Delta Wing Models in Low Subsonic Flow
2. Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow
3. A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model
4. Modeling Aerodynamic Nonlinearities for Two Aeroelastic Configurations: Delta Wing and Flapping Flag
5. Computation of Limit Cycle Oscillations of a Delta Wing
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