Compact Methodology for Computing Limit-Cycle Oscillations in Aeroelasticity
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
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/10.2514/2.6880
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