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li weixuan
li weixuan
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Cited by
Year
Current technologies and challenges of applying fuel cell hybrid propulsion systems in unmanned aerial vehicles
B Wang, D Zhao, W Li, Z Wang, Y Huang, Y You, S Becker
Progress in Aerospace Sciences 116, 100620, 2020
1292020
Evaluation of NOx emissions characteristics in a CO2-Free micro-power system by implementing a perforated plate
T Cai, D Zhao, Y Sun, S Ni, W Li, D Guan, B Wang
Renewable and Sustainable Energy Reviews 145, 111150, 2021
1002021
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
Proper orthogonal and dynamic mode decomposition analyses of nonlinear combustion instabilities in a solid-fuel ramjet combustor
W Li, D Zhao, L Zhang, X Chen
Thermal Science and Engineering Progress 27, 101147, 2022
442022
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
Thermal performances and emitter efficiency improvement studies on premixed micro-combustors with different geometric shapes for thermophotovoltaics applications
S Ni, D Zhao, M Sellier, J Li, X Chen, X Li, F Cao, W Li
Energy 226, 120298, 2021
252021
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
Numerical investigations on solid-fueled ramjet inlet thermodynamic properties effects on generating self-sustained combustion instability
W Li, D Zhao, X Chen, Y Sun, S Ni, D Guan, B Wang
Aerospace Science and Technology 119, 107097, 2021
242021
Hypersonic flow characteristics and relevant structure thermal response induced by the novel combined spike-aerodome and lateral jet strategy
L Zhu, Y Li, X Chen, H Li, W Li, C Li
Aerospace science and technology 95, 105459, 2019
242019
Experimental and model investigation on agglomeration of aluminized fuel-rich propellant in solid fuel ramjet
L Li, X Chen, C Zhou, W Li, M Zhu
Combustion and Flame 219, 437-448, 2020
212020
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
Swirling effect on thermodynamic performance in a solid fueled ramjet with paraffin-polyethylene
W Li, X Chen, D Zhao, B Wang, K Ma, T Cai
Aerospace Science and Technology 107, 106341, 2020
192020
Numerical investigation of inlet thermodynamic conditions on solid fuel ramjet performances
W Li, D Zhao, X Chen, L Zhu, S Ni
International Journal of Aerospace Engineering 2021, 1-20, 2021
152021
Investigation on the effect of diaphragm on the combustion characteristics of solid-fuel ramjet
L Gong, X Chen, H Yang, W Li, C Zhou
Acta Astronautica 139, 449-462, 2017
142017
Unsteady simulation of ignition of turbulent reactive swirling flow of novel design of solid-fuel ramjet motor
O Musa, X Chen, Y Li, W Li, W Liao
Energies 12 (13), 2513, 2019
102019
Numerical investigation of the effect of sudden expansion ratio of solid fuel ramjet combustor with swirling turbulent reacting flow
W Li, X Chen, W Cai, O Musa
Energies 12 (9), 1784, 2019
92019
Establishment process of spiked lateral jet in hypersonic flows
L Zhu, W Li, X Tian, J Song, B Hu
Aerospace Science and Technology 124, 107507, 2022
82022
Combustion characteristics of paraffin-polyethylene blends fuel for solid fuel ramjet
W Li, X Chen, Y Su, O Musa
Journal of Aerospace Engineering 33 (4), 04020043, 2020
82020
Nonablative dual-jet strategy for drag and heat reduction of hypersonic blunt vehicles
L Zhu, X Tian, W Li, M Yan, X Tang, M Huang
Journal of Aerospace Engineering 34 (5), 04021052, 2021
62021
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