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Modeling Technique of the Aircraft Unsteady Aerodynamics Due to the Travelling Gust 被引量:1
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作者 JING Zhiwei TANG Chu 《International Journal of Plant Engineering and Management》 2022年第2期86-102,共17页
The main equations for computing the unsteady aerodynamics of the aircraft undergoing the travelling gust are derived.Research and simulation on a specific example aircraft are performed,the results indicate that the ... The main equations for computing the unsteady aerodynamics of the aircraft undergoing the travelling gust are derived.Research and simulation on a specific example aircraft are performed,the results indicate that the modeling technique of the aircraft unsteady aerodynamics is correct,and it can meet the requirements due to the head⁃on and tail⁃on travelling gusts. 展开更多
关键词 travelling gust elastic aircraft unsteady aerodynamics doublet lattice method
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