Higher-Order Spectral Analysis of Limit Cycle Oscillations of Fighter Aircraft
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34841
Reference15 articles.
1. Comparison of Static and Dynamic Neural Networks for Limit Cycle Oscillation Prediction
2. Nonlinear mechanisms of transonic aeroelastic instability for the F-16
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