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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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:301/80  |  提交时间: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
作者:  刘文;  张陈安;  Wang Xiao-Peng;  Li Jin-Jie;  王发民
Adobe PDF(7528Kb)  |  收藏  |  浏览/下载:319/49  |  提交时间: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
作者:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民);  Ye ZY
浏览  |  Adobe PDF(1916Kb)  |  收藏  |  浏览/下载:523/126  |  提交时间:2020/05/07
Experimental and Numerical Study on Hypersonic Flow over Double-Wedge Configuration 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 9, 页码: 3227-3230
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Yuan CK(苑朝凯);  Wang C(王春);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(207Kb)  |  收藏  |  浏览/下载:445/110  |  提交时间:2018/01/04
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
作者:  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.
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Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
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(764Kb)  |  收藏  |  浏览/下载:329/89  |  提交时间:2017/09/19
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 6, 页码: 1492-1502
作者:  Liu TS;  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA.
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Accurate Measurement of Nonlinear Liquid Sloshing 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 3, 页码: 771-779
作者:  Yang Y;  Liu ZW;  Shi WX;  Huang XF(黄先富);  Liu, ZW (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
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Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 1, 页码: 161-175
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  He, GW (reprint author), Chinese Acad Sci, State Key Lab Nonlinear Mech, Inst Mech, Beijing 100190, Peoples R China.
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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
作者:  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)  |  收藏  |  浏览/下载:1375/490  |  提交时间: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