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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
作者:  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)
浏览  |  Adobe PDF(1265Kb)  |  收藏  |  浏览/下载：240/72  |  提交时间：2015/09/21
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
作者:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
浏览  |  Adobe PDF(1267Kb)  |  收藏  |  浏览/下载：134/44  |  提交时间：2017/06/01
Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet  
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
作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
浏览  |  Adobe PDF(162Kb)  |  收藏  |  浏览/下载：158/71  |  提交时间：2017/06/01
Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
扫描式总压耙在高超声速推进风洞流场测量中的应用 期刊论文
实验流体力学, 2005, 卷号: 19, 期号: 2, 页码: 71-73,83
作者:  常远;  顾洪斌;  陈立红;  张新宇
Adobe PDF(256Kb)  |  收藏  |  浏览/下载：519/149  |  提交时间：2010/05/03
扫描式总压耙  超声速喷管流场  总压分布  马赫数分布  
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
作者:  Chang XY(张新宇);  Gu HB(顾洪斌);  Chen LH(陈立红)
浏览  |  Adobe PDF(139Kb)  |  收藏  |  浏览/下载：163/68  |  提交时间：2017/06/01
Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
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
作者:  陈立红;  张新宇;  顾洪斌
Adobe PDF(347Kb)  |  收藏  |  浏览/下载：635/225  |  提交时间：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  
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
作者:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(4312Kb)  |  收藏  |  浏览/下载：146/62  |  提交时间：2017/06/01
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
作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
Adobe PDF(872Kb)  |  收藏  |  浏览/下载：213/80  |  提交时间：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures