Flutter analysis of a supersonic composite airfoil skin by using the differential quadrature method

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[1] Niu, Yaobin
[2] Wang, Zhongwei
[3] Zhang, Weihua
来源：
Niu, Y. (niuyaobin1234@126.com) | 2012年 / Springer Science and Business Media, LLC卷 / 48期
关键词：
Aeroelasticity; -; Wings; Differentiation; (calculus); Flutter; (aerodynamics);
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