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Experimental and numerical investigation on the longitudinal stage separation for parallel-stage two-stage-to-orbit vehicle 会议论文
34th International Symposium on Shock Waves, 韩国, 16-21 July, 2023
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Favorite  |  View/Download：2/0  |  Submit date：2024/06/04
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
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(556Kb)  |  Favorite  |  View/Download：192/49  |  Submit date：2020/01/06
Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(532Kb)  |  Favorite  |  View/Download：214/78  |  Submit date：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
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
Adobe PDF(4139Kb)  |  Favorite  |  View/Download：314/70  |  Submit date：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
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(6096Kb)  |  Favorite  |  View/Download：345/99  |  Submit date：2018/01/16
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
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(6592Kb)  |  Favorite  |  View/Download：332/82  |  Submit date：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
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(5104Kb)  |  Favorite  |  View/Download：267/52  |  Submit date：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow