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Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：260/89  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(517Kb)  |  收藏  |  浏览/下载：310/100  |  提交时间：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：274/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
作者:  Tong FL(童福林);  Li XL(李新亮);  Duan, Yanhui;  Yu ZP(于长平);  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(3818Kb)  |  收藏  |  浏览/下载：295/117  |  提交时间：2018/01/16
Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:  Yin B(银波);  Yang GW(杨国伟);  Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
浏览  |  Adobe PDF(6552Kb)  |  收藏  |  浏览/下载：251/77  |  提交时间：2018/01/16
Immersed-boundary Method  Micro-air Vehicles  Insect Flight  Vortices  Forces  Flows  
EXPERIMENTAL AND NUMERICAL STUDY OF THE CLOUD CAVITATING FLOW AROUND A SLENDER CYLINDER WITH A PETALS-SHAPED SECTION 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:  Wang YW(王一伟);  Huang J(黄荐);  Xu C(徐畅);  Yu C(余超);  Huang CG(黄晨光);  Wu XC(吴小翠);  Wang, YW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.;  Wang, YW (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(1600Kb)  |  收藏  |  浏览/下载：338/68  |  提交时间：2018/01/16
Large-eddy Simulation  Hydrofoil  Propeller  Surface  
THE AERODYNAMIC CHARACTERISTICS OF THE PANTOGRAPH WHEN THE TRAIN PASSES THROUGH THE TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:  Guo DL(郭迪龙);  Liu W;  Song JH(宋军浩);  Zhang Y;  Yang GW(杨国伟);  Guo, DL (reprint author), Chinese Acad Sci, Inst Mech, Beijing, Peoples R China.
浏览  |  Adobe PDF(1508Kb)  |  收藏  |  浏览/下载：384/93  |  提交时间：2018/01/16