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Omer Musa
Omer Musa
Associate Professor of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics
Verified email at nuaa.edu.cn - Homepage
Title
Cited by
Cited by
Year
Investigation of drag and heat reduction induced by a novel combinational lateral jet and spike concept in supersonic flows based on conjugate heat transfer approach
L Zhu, X Chen, Y Li, O Musa, C Zhou
Acta astronautica 142, 300-313, 2018
582018
Effect of inlet conditions on swirling turbulent reacting flows in a solid fuel ramjet engine
O Musa, C Xiong, Z Changsheng, W Li
Applied Thermal Engineering 113, 186-207, 2017
542017
Numerical investigation on the performance of scramjet combustor with a novel strut configuration
C Li, X Chen, Y Li, O Musa, L Zhu
Applied Thermal Engineering 159, 113894, 2019
442019
Experimental and numerical investigations on the decomposition and combustion characteristics of composite propellant with Mg/Al particles additives
M Zhu, X Chen, C Zhou, J Xu, O Musa, H Xiang
Applied Thermal Engineering 111, 863-875, 2017
402017
Experimental and numerical investigation on the ignition and combustion stability in solid fuel ramjet with swirling flow
O Musa, C Xiong, Z Changsheng
Acta Astronautica 137, 157-167, 2017
392017
Prediction of swirling cold flow in a solid-fuel ramjet engine with a modified rotation/curvature correction SST turbulence model
O Musa, Z Changsheng, C Xiong, G Lunkun
Applied Thermal Engineering 105, 737-754, 2016
392016
The effect of pressure and oxygen concentration on the ignition and combustion of aluminum–magnesium fuel-rich propellant
L Li, X Chen, O Musa, C Zhou, M Zhu
Aerospace science and technology 76, 394-401, 2018
382018
Role of the backward-facing steps at two struts on mixing and combustion characteristics in a typical strut-based scramjet with hydrogen fuel
C Li, X Chen, Y Li, O Musa, L Zhu, W Li
International journal of hydrogen energy 44 (52), 28371-28387, 2019
312019
Combustion characteristics of a novel design of solid-fuel ramjet motor with swirl flow
O Musa, C Xiong, L Weixuan, L Wenhe
Aerospace Science and Technology 92, 750-765, 2019
262019
Numerical and experimental investigation of the effect of geometry on combustion characteristics of solid-fuel ramjet
L Gong, X Chen, O Musa, H Yang, C Zhou
Acta Astronautica 141, 110-122, 2017
262017
Investigation of the effect of geometry of combustor on combustion characteristics of solid-fuel ramjet with swirl flow
W Li, X Chen, O Musa, L Gong, L Zhu
Applied Thermal Engineering 145, 229-244, 2018
252018
Combustion characteristics and turbulence modeling of swirling reacting flow in solid fuel ramjet
O Musa, C Xiong, Z Changsheng
Acta Astronautica 139, 1-17, 2017
252017
Experimental investigation on laser ignition and combustion characteristics of NEPE propellant
LB Li, X Chen, CS Zhou, M Zhu, O Musa
Propellants, Explosives, Pyrotechnics 42 (9), 1095-1103, 2017
242017
Experimental investigation on the effect of swirling flow on combustion characteristics and performance of solid fuel ramjet
O Musa, L Weixuan, C Xiong, G Lunkun, L Wenhe
Acta Astronautica 148, 163-174, 2018
212018
Assessment of the modified rotation/curvature correction SST turbulence model for simulating swirling reacting unsteady flows in a solid-fuel ramjet engine
O Musa, C Xiong, Z Changsheng, G Lunkun
Acta Astronautica 129, 241-252, 2016
202016
Verification study of a cfd-rans code for turbulent flow at high reynolds numbers
O Musa, Z Changshen, C Xiong, L Yingkun
International Journal of Modeling and Optimization 6 (1), 1, 2016
172016
Numerical study of micron-scale aluminum particle combustion in an afterburner using two-way coupling CFD–DEM approach
M Zhu, X Chen, C Zhou, J Xu, O Musa
Flow, Turbulence and Combustion 105, 191-212, 2020
152020
Three-dimensional multi-physics coupled simulation of ignition transient in a dual pulse solid rocket motor
Y Li, X Chen, J Xu, C Zhou, O Musa
Acta Astronautica 146, 46-65, 2018
152018
Experimental and numerical investigations of the effect of pressure and oxygen concentration on combustion characteristics of Al/Mg fuel-rich propellants
L Li, X Chen, C Zhou, M Zhu, O Musa
Applied Thermal Engineering 167, 114695, 2020
142020
Investigations on the influence of swirl intensity on solid-fuel ramjet engine
O Musa, C Xiong, Z Chang-sheng, L Ying-kun, L Wen-He
Computers & Fluids 167, 82-99, 2018
122018
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