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Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Li GL(李广利);  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ(徐应洲)
浏览  |  Adobe PDF(664Kb)  |  收藏  |  浏览/下载：377/89  |  提交时间：2018/01/16
Aerodynamics  Angle Of Attack  Angle Of Attack Indicators  Boundary Layers  Drag  Drag Coefficient  High Pressure Effects  Hypersonic Aerodynamics  Hypersonic Flow  Spacecraft  
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Xiao Y(肖尧);  Cui K(崔凯);  Li GL(李广利);  Xu YZ(徐应洲)
浏览  |  Adobe PDF(639Kb)  |  收藏  |  浏览/下载：274/88  |  提交时间：2018/01/16
Aerodynamics  Air Engines  Aspect Ratio  Computational Fluid Dynamics  Drag  Engines  Hypersonic Aerodynamics  Lift  Lift Drag Ratio  Propulsion  Spacecraft  Vehicles  
Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Xu YZ(徐应洲);  Cui K(崔凯);  Li GL(李广利);  Xiao Y(肖尧)
浏览  |  Adobe PDF(461Kb)  |  收藏  |  浏览/下载：303/83  |  提交时间：2018/01/16
Aerodynamic Configurations  Aerodynamics  Computational Fluid Dynamics  Deformation  Evolutionary Algorithms  Fluid Dynamics  Hypersonic Aerodynamics  Optimization  Spacecraft  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
浏览  |  Adobe PDF(468Kb)  |  收藏  |  浏览/下载：292/81  |  提交时间：2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere 会议论文
International Symposium on Infrared Technology and Application / International Symposium on Robot Sensing and Advanced Control, Beijing, PEOPLES R CHINA, MAY 09-11, 2016
作者:  Wu J;  Yu XL(余西龙);  Zhu XJ;  Ma J;  Mao HX;  Wu, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wu, J (reprint author), Sci & Technol Opt Radiat Lab, Beijing 100854, Peoples R China.
浏览  |  Adobe PDF(1160Kb)  |  收藏  |  浏览/下载：272/82  |  提交时间：2017/05/12
Hypersonic  Mid-infrared  Atom  Diatomic Molecule  Partition-functions  Molecules  Air  
Monte Carlo modeling of electron density in hypersonic rarefied gas flows 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18, 2014
作者:  Fan J(樊菁);  Zhang YH(张羽淮);  Jiang JZ(蒋建政)
浏览  |  Adobe PDF(835Kb)  |  收藏  |  浏览/下载：660/175  |  提交时间：2015/01/21
Hypersonic Rarefied Gas Flow  Electron Density  Dsmc  Tss  Ram-c Ii Flight Test  
An Investigation of Grid Resolution on Hypersonic Viscous Flow Simulation 会议论文
1st International High-Speed Flow Conference, Beijing, May 13-14, 2014
作者:  Sun QH(孙泉华);  Zhu HY(朱辉玉);  Su TF(苏腾飞)
浏览  |  Adobe PDF(1203Kb)  |  收藏  |  浏览/下载：743/128  |  提交时间：2015/01/01
Hypersonic Viscous Flow  Grid Resolution  Cfd  Truncated Error  
The Basis of an Industry-standard Aerodynamic Computation and its Theoretical Basis with Inferences and Applications 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Gao Z(高智)
浏览  |  Adobe PDF(780Kb)  |  收藏  |  浏览/下载：535/150  |  提交时间：2014/03/11
Numerical Simulation  Hypersonic Flow  Viscous-inviscid Interacting Shear Flow (Isf)  Cfd Validation  Wall Momentum-energy Criteria  
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Wang FM(王发民);  Han HQ(韩汉桥);  Lei MF(雷麦芳);  Zhang J(张杰);  Wang FM(王发民)
浏览  |  Adobe PDF(3663Kb)  |  收藏  |  浏览/下载：538/139  |  提交时间：2014/03/11
Hypersonic  Aerothermal Protection  Power-law Leading Edge  Aerodynamic Performance  
A New Non-ablative TPS for Hypersonic Vehicles 会议论文
第十五届全国激波与激波管学术会议（上册）, 中国浙江杭州, 2012-07-13
作者:  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(985Kb)  |  收藏  |  浏览/下载：177/56  |  提交时间：2015/09/10
Hypersonic Flow  Tps  Shock Wave  Drag Reduction