Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
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  
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
Authors:  常远;  顾洪斌;  陈立红;  张新宇
Adobe PDF(256Kb)  |  Favorite  |  View/Download：554/161  |  Submit date：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
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  
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  
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)
View  |  Adobe PDF(4312Kb)  |  Favorite  |  View/Download：173/70  |  Submit date：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
Authors:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：235/86  |  Submit date：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures