Prediction of Aeroelastic Limit-Cycle Oscillations Based on Harmonic Forced-Motion Oscillations
Author:
Affiliation:
1. DLR, German Aerospace Center, 37073 Göttingen, Germany
2. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055852
Reference33 articles.
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5. KuznetsovY., Elements of Applied Bifurcation Theory, Vol. 112, 2nd ed., Springer–Verlag, New York, 1998, pp. 88–89.
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