Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
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DOI:
10.2514/6.2004-1696
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发表时间:
2004-04
影响因子:
10
通讯作者:
Jeffrey P. Thomas;E. Dowell;K. Hall;C. Denegri
中科院分区:
文献类型:
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作者:
Jeffrey P. Thomas;E. Dowell;K. Hall;C. Denegri