Limit Cycle Oscillations of Delta Wing Models in Low Subsonic Flow
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.627
Reference11 articles.
1. Dowell, E. H., Aeroelasticity of Plates and Shells, Kluwer, Dordrecht, TheNetherlands,1975, pp.35-44.'
2. AN OVERVIEW OF AEROELASTICITY STUDIES FOR THE NATIONAL AERO-SPACE PLANE
3. Limited amplitude panel flutter with a temperature differential
4. Limit cycle oscillation of a fluttering cantilever plate
5. Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow
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