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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:448/110  |  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:332/90  |  提交时间:2017/09/19
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:1379/493  |  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  
Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone 期刊论文
AIAA Journal, 2008, 页码: 2899-2913
作者:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Lab Nonlinear Mech, Beijing 100080, Peoples R China.
Adobe PDF(11335Kb)  |  收藏  |  浏览/下载:906/209  |  提交时间:2009/08/03
Hyperbolic Conservation-laws