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Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
Authors:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(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  
Experimental Studies on Model Scramjet in a Mach 6 High Enthalpy Free-Jet Wind Tunnel 会议论文
The 24th International Symposium on Shock Waves, Beijing, 2004-07-11
Authors:  Zhang XY(张新宇);  Chen LH(陈立红);  Gu HB(顾洪斌);  Yu G(俞刚);  Zhang XY(张新宇)
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Direct initiation of detonation with ignition tube 会议论文
24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA, Beijing, PEOPLES R CHINA, JUL 11-16, 2004
Authors:  Chen H(陈宏);  Zhang XY(张新宇);  Yu HR(俞鸿儒);  Chen H(陈宏)
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Direct Initiation of Detonation by Ignition Tube 会议论文
24th International Symposium on Shock Waves, Beijing, China, 2004
Authors:  Chen H(陈宏);  Zhang XY(张新宇);  Yu HR(俞鸿儒)
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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
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超音速冲压喷气发动机  超高速风洞  超声速扩压段  模型  
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