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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:182/73  |  Submit date:2017/06/01
Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets