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Wei Qian
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Professor Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Patents
[1] 一种模拟全动舵面颤振模型弯扭支撑刚度的装置
[2] 一种用于超声速风洞全动舵面模型的多功能根肋
[3] 颤振风洞模型的全动舵面与弹性机身两铰点弹性连接系统
[4] 一种全动平尾跨音速颤振风洞试验模型方案
[5] 一种中央固支的后机身尾翼低速颤振模型
[6] 一种低超重比复合材料翼面颤振模型
[7] 一种飞机颤振模型的频率误差修正方法
[8] 一种调整热压罐内流场温度均匀性的方法
TOTAL 8 PIECE 1/1
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