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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229./通讯作者：Wang YP(汪运鹏)(1,2)
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：696/108  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946./通讯作者：Wang YP(汪运鹏)(1,2)
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：390/112  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan([email protected])
View  |  Adobe PDF(566Kb)  |  Favorite  |  View/Download：397/88  |  Submit date：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Concept of non-ablative thermal protection system for hypersonic vehicles 期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
Authors:  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)  |  Favorite  |  View/Download：1474/531  |  Submit date：2013/04/07
Flow Fields  Flow Visualization  Hypersonic Aerodynamics  Hypersonic Vehicles  Mach Number  Shock Waves  Thermal Insulating Materials  Engineering Applications  Experimental Datum  Hypersonic Wind Tunnels  Numerical Results  Stagnation Points  Thermal Protection  Thermal Protection System  Working Pressures  
Experimental and computational investigation of a full aircraft flutter at transonic speeds 会议论文
International Forum on Aeroelasticity and Structural Dynamics, IFASD 2013, Bristol, United kingdom, June 24, 2013 - June 27, 2013
Authors:  Qian W;  Yang GW(杨国伟);  Luo JG;  Yang R;  Zhang GJ
Favorite  |  View/Download：205/0  |  Submit date：2018/11/08
Aeroelasticity  Aircraft manufacture  Airframes  Computational fluid dynamics  Elastic waves  Flutter (aerodynamics)  Structural dynamics  Supersonic aircraft  Transonic aerodynamics  Viscous flow  Wind stress  Wind tunnels  Aircraft structure  CFD simulations  CFD/CSD  Computational investigation  Flutter boundary predictions  Transonic flutter  Unsteady aerodynamics  Wind tunnel tests  
Aerodynamic design on China new high-speed trains 会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
Authors:  Yang GW(杨国伟);  Yang GW(杨国伟)
Adobe PDF(553Kb)  |  Favorite  |  View/Download：814/264  |  Submit date：2013/02/06
Railroad Cars  Railroad Transportation  Railroad Tunnels  Railroads  Wind Effects  Aerodynamic Designs  Aerodynamic Noise  Aerodynamic Performance  Cross-wind Effects  High Speed Trains  Pressure Waves  Running Conditions  Running Tests  Running-in  Wind Tunnel Experiment