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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
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：325/86  |  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  
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider 期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
Authors:  刘文;  张陈安;  Wang Xiao-Peng;  Li Jin-Jie;  王发民
Adobe PDF(7528Kb)  |  Favorite  |  View/Download：373/56  |  Submit date：2021/08/30
Design and Optimization Method for Hypersonic Quasi-Waverider 期刊论文
AIAA Journal, 2020, 卷号: 58, 期号: 5, 页码: 2132-2146
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民);  Ye ZY
View  |  Adobe PDF(1916Kb)  |  Favorite  |  View/Download：544/128  |  Submit date：2020/05/07
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1329Kb)  |  Favorite  |  View/Download：609/120  |  Submit date：2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
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：1397/500  |  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  
Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels 期刊论文
AIAA Journal, 2002, 卷号: 40, 期号: 10, 页码: 2009-2016
Authors:  Jiang ZL(姜宗林);  Zhao W(赵伟);  Wang C(王超);  Takayama K;  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gasdynam, Beijing 100080, Peoples R China.
View  |  Adobe PDF(288Kb)  |  Favorite  |  View/Download：1094/293  |  Submit date：2007/06/15
Second-order thickness terms in unsteady wing theory 期刊论文
AIAA Journal, 1986, 卷号: 24, 期号: 10, 页码: 1702-1703
Authors:  Gu WK(顾为凯)
Adobe PDF(253Kb)  |  Favorite  |  View/Download：500/101  |  Submit date：2009/08/03