Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                                
Selected(0)Clear Items/Page:    Sort:
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
View  |  Adobe PDF(759Kb)  |  Favorite  |  View/Download：574/187  |  Submit date：2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network  
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:  Li F(李飞);  Yu XL(余西龙);  Gu HB(顾洪斌);  Li Z(李智);  Chen LH(陈立红);  Zhang XY(张新宇);  Li F(李飞)
View  |  Adobe PDF(420Kb)  |  Favorite  |  View/Download：606/203  |  Submit date：2014/02/24
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:  Gu HB(顾洪斌);  Li Z(李智);  Li F(李飞);  Chen LH(陈立红);  Gu SL(顾声龙);  Zhang XY(张新宇);  Gu HB(顾洪斌)
View  |  Adobe PDF(242Kb)  |  Favorite  |  View/Download：559/211  |  Submit date：2014/02/24
超声速燃烧中气动斜坡的研究 会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
Authors:  卫喆;  陈立红;  顾洪斌;  李飞;  顾声龙;  张新宇
Adobe PDF(569Kb)  |  Favorite  |  View/Download：584/152  |  Submit date：2010/11/25
超燃冲压发动机  气动斜坡  直连式实验台  散射  
Performance of the fuel injector in supersonic combustor 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙);  Chang XY(张新宇);  Wei, Z. (weizhejiji@yahoo.com.cn)
View  |  Adobe PDF(167Kb)  |  Favorite  |  View/Download：184/60  |  Submit date：2017/07/14
Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors  
Flow-field of the excited jet and mixing in the supersonic flow 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:  Gu SL(顾声龙);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Wei Z(卫喆);  Chang XY(张新宇);  Gu, S. (gushenglong@imech.ac.cn)
View  |  Adobe PDF(261Kb)  |  Favorite  |  View/Download：230/74  |  Submit date：2017/07/14
Different Frequency  Gas Sampling  Hartmann  Jet Devices  Large-scale Structure  Planar Laser  Shear Layer  Total-pressure Loss