| Citation: | DENG Wei-xin, LE Jia-ling, YANG Shun-hua, TIAN Ye, ZHANG Wan-zhou, XU Ming-heng. Effect of fueling scheme on scramjet combustion performance[J]. Journal of Aerospace Power, 2013, 28(7): 1449-1457.
|
| [1] |
Cabell K,Hass N,Storch A,et al.HIFiRE direct-connect rig (HDCR) phase:I scramjet test results from the NASA langley arc-heated scramjet test facility [R].AIAA-2011-2248,2011.
|
| [2] |
XU Jinglei,MA Jing,GU Rui,et al.PIV experimental and numerical investigation of cold flowfield of scramjet combustor with inlet/isolator [R].AIAA-2011-2312,2011.
|
| [3] |
房田文,丁猛,周进.凹腔超声速流场结构的试验研究[J].国防科技大学学报,2007,29(3):1-5. FANG Tianwen,DINGMeng,ZHOU Jin.Experimental investigation on supersonic flows over cavities[J].Journal of National University of Defense Technology,2007,29(3):1-5.(in Chinese)
|
| [4] |
LI Qing,PAN Yu,TAN Janguo,et al.Experiment research of ramjet with cavity-based flameholder [R].AIAA-2009-5049,2009.
|
| [5] |
Lin K C,Tam C J,Boxx I,et al.Flame characteristics and fuel entrainment inside a cavity flame holder in a scramjet combustor [R].AIAA-2007-5381,2007.
|
| [6] |
Hatakeyama R,Tomioka S,Izumikawa M,et al.Research on combustion of hydrocarbon fuel in a supersonic combustor [R].AIAA-2010-7038,2010.
|
| [7] |
Retaureau G J,Menon S.Experimental studies on flame stability of a fueled cavity in a supersonic crossflow [R].AIAA-2010-6718,2010.
|
| [8] |
Ghodke C D,Pranatharthikarany J,Retaureauz G J,et al.Numerical and experimental studies of flame stability in a cavity stabilized hydrocarbon-fueled scramjet [R].AIAA-2011-2365,2011.
|
| [9] |
SUN Mingbo,WANG Hongbo,BAI Xuesong,et al.Experimental and numerical study on flame stabilization in a supersonic combustor with hydrogen injection upstream of cavity flameholders [R].AIAA-2009-5187,2009.
|
| [10] |
Laurence S J,Schramm J M,Karl S,et al.An experimental investigation of steady and unsteady combustion phenomena in the hyshot:Ⅱ combustor [R].AIAA-2011-2310,2011.
|
| [11] |
Mitani T,Kouchi T.Flame structures and combustion efficiency computed for a Mach 6 scramjet engine[J].Combustion and Flame,2005,142(1):187-196.
|
| [12] |
LI Junhong,SHEN Qing,CHENG Xiaoli,et al.Investigation of equivalence ratio effect on kerosene-fueled low internal drag scramjet combustor performance [R].AIAA-2011-2246,2011.
|
| [13] |
Donbar J M,Linn G J,Srikant S,et al.High-frequency pressure measurements for unstart detection in scramjet isolators [R].AIAA-2010-6557,2010.
|
| [14] |
Micka D J, Driscoll J F.Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder[J].Proceedings of the Combustion Institute,2009,32(2):2397-2404.
|
| [15] |
Heiser W H,Pratt D T,Daley D H, et al.Hypersonic airbreathing propulsion[M].Washington,DC:American Institute of Aeronautics and Astronautics Incorporarion,1994.
|
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