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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 |