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Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
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Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
壁面凹腔强化H2超声速燃烧的数值模拟 期刊论文
推进技术, 2006, 期号: 6, 页码: 563-567
Authors:  陈方;  陈立红;  张新宇
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Research on three-dimensional scramiet inlet 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
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Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet  
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)
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Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
Analyses of supersonic combustion by gas sampling 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:  Chen LH(陈立红);  Lin R;  Gu HB(顾洪斌);  Chang XY(张新宇)
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Combustion Efficiency  Gas Sampling  Probe Sampling  Scramjet  
Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
Authors:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
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Compressible Navier-stokes  Computational Studies  Experimental Comparison  Experimental Investigations  Flow Charac-teristics  Hypersonic Propulsion Test Facility  Performance Parameters  Scramjet Inlets  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
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Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
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Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors