基于主动控制策略的机翼颤振特性模拟
刘楚源,刘泽森,宋汉文(
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THE SIMULATION OF AIRFOIL FLUTTER CHARACTERISTIC BASED ON ACTIVE CONTROL STRATEGY
Chuyuan Liu,Zesen Liu,Hanwen Song()
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图4. 非自伴随系统与Nastran对比
Fig.4. Comparison between non-self-adjoint system and Nastran
