Ming Bo Sun
TítuloCitado porAño
Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder
MB Sun, ZG Wang, JH Liang, H Geng
Journal of Propulsion and Power 24 (4), 688-696, 2008
1102008
Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor
H Wang, Z Wang, M Sun, H Wu
International journal of hydrogen energy 38 (27), 12078-12089, 2013
1052013
Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition
MB Sun, C Gong, SP Zhang, JH Liang, WD Liu, ZG Wang
Experimental Thermal and Fluid Science 43, 90-96, 2012
912012
Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder
H Wang, Z Wang, M Sun, N Qin
Proceedings of the combustion institute 34 (2), 2073-2082, 2013
802013
Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor
Z Wang, M Sun, H Wang, J Yu, J Liang, F Zhuang
Proceedings of the Combustion Institute 35 (2), 2137-2144, 2015
722015
Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity
H Wang, Z Wang, M Sun, N Qin
Acta Astronautica 108, 119-128, 2015
592015
Review of cavity-stabilized combustion for scramjet applications
Z Wang, H Wang, M Sun
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014
572014
Characteristics of oscillations in supersonic open cavity flows
H Wang, M Sun, N Qin, H Wu, Z Wang
Flow, turbulence and combustion 90 (1), 121-142, 2013
552013
Mixing characteristics in a supersonic combustor with gaseous fuel injection upstream of a cavity flameholder
M Sun, H Geng, J Liang, Z Wang
Flow, turbulence and combustion 82 (2), 271-286, 2009
552009
Large eddy simulation based studies of jet–cavity interactions in a supersonic flow
H Wang, Z Wang, M Sun, N Qin
Acta Astronautica 93, 182-192, 2014
462014
Large Eddy Simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity
Z Cai, X Liu, C Gong, M Sun, Z Wang, XS Bai
Acta Astronautica 126, 375-381, 2016
402016
Large-Eddy/Reynolds-averaged Navier–Stokes simulation of combustion oscillations in a cavity-based supersonic combustor
H Wang, Z Wang, M Sun, N Qin
international journal of hydrogen energy 38 (14), 5918-5927, 2013
402013
Experimental and three-dimensional numerical investigations on H2/air continuous rotating detonation wave
SJ Liu, ZY Lin, WD Liu, W Lin, MB Sun
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2013
402013
Experimental investigation on transverse jet penetration into a supersonic turbulent crossflow
MB Sun, SP Zhang, YH Zhao, YX Zhao, JH Liang
Science China Technological Sciences 56 (8), 1989-1998, 2013
372013
A hybrid LES (Large Eddy Simulation)/assumed sub-grid PDF (Probability Density Function) model for supersonic turbulent combustion
HB Wang, N Qin, MB Sun, HY Wu, ZG Wang
Science China Technological Sciences 54 (10), 2694, 2011
362011
Experimental investigation on ignition schemes of a supersonic combustor with the rearwall-expansion cavity
Z Cai, Y Yang, M Sun, Z Wang
Acta Astronautica 123, 181-187, 2016
342016
Thrust vectoring of a continuous rotating detonation engine by changing the local injection pressure
L Shi-Jie, L Zhi-Yong, S Ming-Bo, L Wei-Dong
Chinese Physics Letters 28 (9), 094704, 2011
342011
Large Eddy Simulation of the flame stabilization process in a scramjet combustor with rearwall-expansion cavity
Z Wang, Z Cai, M Sun, H Wang, Y Zhang
International Journal of Hydrogen Energy 41 (42), 19278-19288, 2016
312016
Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor
M Sun, Z Zhong, J Liang, H Wang
Acta Astronautica 127, 112-119, 2016
312016
Effect of combustor geometry and fuel injection scheme on the combustion process in a supersonic flow
Z Cai, Z Wang, M Sun, XS Bai
Acta Astronautica 129, 44-51, 2016
302016
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
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