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Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
作者:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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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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Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载:469/171  |  提交时间:2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
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
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
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.
浏览  |  Adobe PDF(5500Kb)  |  收藏  |  浏览/下载:330/103  |  提交时间:2015/03/17