Flow Angle, Temperature and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary

机译：超音速面板颤振稳定性边界上的流动角，温度和气动阻尼

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;AIAA/ASME/AHS Adaptive Structures Conference;AIAA Non-Deterministic Approaches Forum;AIAA Gossamer Spacecraft Forum》|2002年|P.1-11|共11页
会议地点 Denver, CO(US);Denver, CO(US);Denver, CO(US);Denver, CO(US)
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G. Cheng; C. Mei; Y. Lee;
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Old Dominion University Norfolk VA;

City University of Hong Kong Hong Kong China (prc);

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1. Flow Angle, Temperature, and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary [J] . Guangfeng Cheng, Y. Y. Lee, Chuh Mei Journal of Aircraft . 2003,第2期

机译：超音速面板颤振稳定性边界上的流动角，温度和气动阻尼
2. Effects of hysteretic and aerodynamic damping on supersonic panel flutter of composite plates [J] . Koo KN, Hwang WS Journal of Sound and Vibration . 2004,第3期

机译：滞后和气动阻尼对复合板超声面板颤振的影响
3. Interaction of panel flutter with inviscid boundary layer instability in supersonic flow [J] . Vasily Vedeneev Journal of Fluid Mechanics . 2013,第Null期

机译：超音速流动中面板颤振与边界层不粘稠的相互作用
4. Flow Angle, Temperature and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society/ASC Structures, Structural Dynamics, and Materials Conference . 2002

机译：超声波面板颤动稳定边界的流量，温度和空气动力学阻尼
5. Nonlinear flutter of curved panels under yawed supersonic flow using finite elements. [D] . Azzouz, Mohamed Salim. 2005

机译：偏航超声速作用下曲面板的非线性颤振，采用有限元方法。
6. On the Stability of MHD Boundary Layer Flow over a Stretching/Shrinking Wedge [O] . Izyan Syazana Awaludin, Anuar Ishak, Ioan Pop -1

机译：拉伸/收缩楔块上MHD边界层流的稳定性
7. A Combined Energy Method for Flutter Instability Analysis of Weakly Damped Panels in Supersonic Airflow [O] . Xiaochen Wang, Zhichun Yang, Guiwei Zhang, 2021

机译：超声波气流弱阻尼板颤动稳定性分析的组合能量法
8. Thermoelastic Damping and Its Effect on Flutter of Stressed Panels Situated in a Supersonic Airflow [R] . Shieh, R. C. 1971

机译：热弹性阻尼及其对超音速气流中受应力板颤振的影响

Flow Angle, Temperature and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary

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