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Influence of rectangular strips size on aerodynamic performance of a high-speed train subjected to crosswind 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者:  Wang MY(王梦莹);  Sun ZX(孙振旭);  Ju SJ(鞠胜军);  Yang GW(杨国伟)
Adobe PDF(1369Kb)  |  收藏  |  浏览/下载:227/79  |  提交时间:2021/11/30
Aerodynamic performance  Crosswind  High-speed train  Orthogonal design  Rectangular strips  Variance analysis  
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者:  Yao W(姚卫);  Chen L(陈留)
Adobe PDF(2272Kb)  |  收藏  |  浏览/下载:256/143  |  提交时间:2021/06/11
高超声速激波边界层干扰研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
作者:  姜文清;  韩桂来;  姜宗林
浏览  |  Adobe PDF(966Kb)  |  收藏  |  浏览/下载:367/106  |  提交时间:2019/11/21
高超声速  激波  边界层  
Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(714Kb)  |  收藏  |  浏览/下载:30/15  |  提交时间:2023/03/17
Aerodynamic Force Measurement in a Large-Scale Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(556Kb)  |  收藏  |  浏览/下载:156/39  |  提交时间:2020/01/06
Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(523Kb)  |  收藏  |  浏览/下载:455/52  |  提交时间:2020/01/06
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载:305/99  |  提交时间:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载:304/87  |  提交时间:2018/01/16
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  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity 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:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载:382/67  |  提交时间:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis