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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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Lift enhancement by bats' dynamically changing wingspan 期刊论文
Journal of Royal Society Inerface, 2015, 卷号: 12, 页码: 20150821
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  He GW(何国威)
浏览  |  Adobe PDF(1708Kb)  |  收藏  |  浏览/下载:437/87  |  提交时间:2016/01/07
Bat Flight  Flapping Flight  Dynamically Changing Wingspan  Unsteady Aerodynamics  
An airplane jig shape design method based on high fidelity aeroelastic simulation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
作者:  Yang W;  Wang QF;  Zhou L;  Zheng GN(郑冠男);  Liu W;  Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Aeroelasticity  Cfd  Csd  Jig Shape  Structural Mesh  
An effective CFD approach for marine-vehicle maneuvering simulation based on hybrid reference frames method 期刊论文
Ocean Engineering, 2015, 卷号: 109, 页码: 83–92
作者:  Wu XC(吴小翠);  Wang YW(王一伟);  Huang CG(黄晨光);  Hu ZQ;  Yi RW
浏览  |  Adobe PDF(851Kb)  |  收藏  |  浏览/下载:378/161  |  提交时间:2016/01/07
Maneuvering Characteristics  Hybrid Reference Frames Method  Rotating Arm Test  Suboff Model  
A novel method of evaluating the lift force on the bluff body based on Noca's flux equation 期刊论文
CHINESE PHYSICS B, 2015, 卷号: 24, 期号: 8, 页码: 84701
作者:  Sui XK(隋相坤);  Jiang N(姜楠);  Sui, XK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Flux Equation  Lift Force  Experimental Error  
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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Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
作者:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(532Kb)  |  收藏  |  浏览/下载:631/152  |  提交时间:2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
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:474/173  |  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  
The Lift Problem in Flapping Forward Flight at Low Reynolds Numbers 会议论文
53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida, USA, Jan 1-5,2015
作者:  Liu TS;  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威)
浏览  |  Adobe PDF(1670Kb)  |  收藏  |  浏览/下载:298/86  |  提交时间:2016/01/07