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Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang Q(汪球);  Lu P(卢盼);  Li JW(栗继伟);  Wu S(吴松);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
Adobe PDF(299Kb)  |  收藏  |  浏览/下载：83/33  |  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：160/42  |  提交时间：2020/01/06
Hypervelocity Test with a Detonation-Driven Expansion Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭峻);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(297Kb)  |  收藏  |  浏览/下载：186/64  |  提交时间：2020/01/06
The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Li XD(李旭东);  Shi CM(师曾敏)
浏览  |  Adobe PDF(376Kb)  |  收藏  |  浏览/下载：338/63  |  提交时间：2020/01/06
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
浏览  |  Adobe PDF(4139Kb)  |  收藏  |  浏览/下载：271/57  |  提交时间：2019/04/19
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：308/89  |  提交时间：2018/01/16
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：386/68  |  提交时间：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
作者:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(764Kb)  |  收藏  |  浏览/下载：351/98  |  提交时间：2016/06/28
Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文
34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
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(6592Kb)  |  收藏  |  浏览/下载：305/78  |  提交时间：2017/05/05
Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(5104Kb)  |  收藏  |  浏览/下载：239/45  |  提交时间：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow