Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
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American Institute of Aeronautics and Astronautics
Cited by 27 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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4. The Computing of Dynamic Derivatives of Hypersonic Lift Body Based on Time Spectral Method;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02
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