Unsteady Unified Hypersonic- Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity

机译：非稳态统一超音速-超音速空气动力学：稳定性和气动弹性的分析方法

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《AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference;AIAA Non-Deterministic Approaches Forum;AIAA/ASME/AHS Adaptive Structures Conference;AIAA Gossamer Spacecraft Forum;AIAA Dynamics Specialists Conference》|2003年|P.1-18|共18页
会议地点 Norfolk, VA(US);Norfolk, VA(US);Norfolk, VA(US);Norfolk, VA(US);Norfolk, VA(US)
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W. Hui; D. Liu;
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Hong Kong University of Science and Technology Hong Kong Hong Kong;

ZONA Technology Scottsdale AZ;

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1. Unsteady Unified Hypersonic/Supersonic Method for Aeroelastic Applications Including Wave/Shock Interaction [J] . Frank R. Chavez, D. D. Liu AIAA Journal . 1995,第6期

机译：包括波浪/冲击相互作用在内的气动弹性非定常统一超音速/超音速方法
2. Unsteady supersonic aerodynamics based on BEM, including thickness effects in aeroelastic analysis [J] . N. Soltani, V. Esfahanian, H. Haddadpour, Journal of Fluids and Structures . 2004,第6期

机译：基于BEM的非定常超声速空气动力学，包括气动弹性分析中的厚度效应
3. Aeroelasticity consideration of supersonic vehicle using closed form analytical aerodynamic model [J] . Fathi Jegarkandi Mohsen Salezadeh Nobari Ali Sabzehparvar Mahdi Haddadpour Hassan Tavakkoli Farhad Aircraft Engineering and Aerospace Technology . 2009,第2期

机译：基于封闭形式解析空气动力学模型的超音速飞行器气动弹性考虑
4. Unsteady Unified Hypersonic- Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society Structures, Structural Dynamics, and Materials Conference . 2003

机译：不稳定统一超音速 - 超音速空气动力学：稳定性和空气弹性的分析与方便方法
5. New acceleration potential method for supersonic unsteady aerodynamics of lifting surfaces, further extension of the nonplanar supersonic doublet point method, and nonlinear, nongradient optimized rational function approximations for supersonic, transient response unsteady aerodynamics. [D] . Tewari, Ashish. 1992

机译：用于提升表面的超音速非稳态空气动力学的新的加速势方法，非平面超音速双重点方法的进一步扩展以及用于超音速，瞬态响应非稳态空气动力学的非线性，非梯度优化有理函数逼近。
6. AEROM: NASA’s Unsteady Aerodynamic and Aeroelastic Reduced-Order Modeling Software [O] . Walter A. Silva -1

机译：AEROM：NASA的非稳态气动和气动弹性降序建模软件
7. Current status of computational methods for transonic unsteady aerodynamics and aeroelastic applications [O] . Malone John B., Edwards John W. 1992

机译：跨音速非定常空气动力学和气动弹性应用计算方法的现状
8. Unsteady Aerodynamics Inputs for Aeroelastic Analyses. Part a: A General Introduction. Part B: Prediction of the Unsteady Airloads on Oscillating Lifting Systems and Bodies in Subsonic and Supersonic Flow [R] . Geissler, W. 1980

机译：气动弹性分析的非定常空气动力学输入。第一部分：概述。 B部分：亚音速和超音速流中摆动提升系统和体的非定常空气载荷预测

Unsteady Unified Hypersonic- Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity

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