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Control Of Vortex Shedding From A Square Cylinder 期刊论文
AIAA Journal, 2008, 页码: 397-407
Authors:  Shao CP(邵传平);  Wei QD;  Shao, CP (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Spatially Developing Flows  
Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone 期刊论文
AIAA Journal, 2008, 页码: 2899-2913
Authors:  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.
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Hyperbolic Conservation-laws  
Performance of supersonic model combustors with distributed injection of supercritical kerosene 会议论文
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United states, July 8, 2007 - July 11, 2007
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Lu XN;  Sung CJ
Adobe PDF(423Kb)  |  Favorite  |  View/Download：223/84  |  Submit date：2017/06/01
Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors  
Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers 会议论文
45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2007-1-8~2007-1-11
Authors:  Tama M;  Wang ZJ;  Rajagopalan G;  Hu H;  He GW(何国威)
Adobe PDF(4409Kb)  |  Favorite  |  View/Download：2036/717  |  Submit date：2012/02/13
Control of Mean and Fluctuating Forces on a Circular Cylinder at High Reynolds Numbers 期刊论文
Acta Mechanica Sinica, 2007, 卷号: 23, 期号: 2, 页码: 133-143
Authors:  Shao CP(邵传平);  Wang JM(王建明);  Shao, CP (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Experimental investigation of cavity-based scramjet model 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
View  |  Adobe PDF(162Kb)  |  Favorite  |  View/Download：188/81  |  Submit date：2017/06/01
Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
Thrust and drag of a scramjet model with different combustor geometries 会议论文
13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 16, 2005 - May 20, 2005
Authors:  Chang XY(张新宇);  Gu HB(顾洪斌);  Chen LH(陈立红)
View  |  Adobe PDF(139Kb)  |  Favorite  |  View/Download：200/82  |  Submit date：2017/06/01
Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
锥形轴对称微管道内流动特性实验研究 期刊论文
应用力学学报, 2004, 卷号: 21, 期号: 2, 页码: 125-128
Authors:  徐征;  李战华;  刘冲;  崔海航;  王立鼎
Adobe PDF(294Kb)  |  Favorite  |  View/Download：676/191  |  Submit date：2007/06/15
显微注射  微流动  锥形管道  流量特性  
扩压段对高超声速推进风洞起动的影响 期刊论文
推进技术, 2004, 卷号: 25, 期号: 5, 页码: 430-434
Authors:  陈立红;  张新宇;  顾洪斌
Adobe PDF(347Kb)  |  Favorite  |  View/Download：685/234  |  Submit date：2007/06/15
超音速冲压喷气发动机  超高速风洞  超声速扩压段  模型  
On the computation of space-time correlations by large-eddy simulation 期刊论文
Physics of Fluids, 2004, 卷号: 16, 期号: 11, 页码: 3859-3867
Authors:  He GW(何国威);  Wang M;  Lele SK;  He, GW (reprint author), Stanford Univ, Ctr Turbulence Res, NASA, Ames Res Ctr, MS 19-44, Moffett Field, CA 94035 USA.
Adobe PDF(147Kb)  |  Favorite  |  View/Download：923/231  |  Submit date：2009/08/03
Isotropic Turbulence  Noise  Sound  Scales