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Han Peng
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Year
Effects of jet in crossflow on flame acceleration and deflagration to detonation transition in methane–oxygen mixture
H Peng, Y Huang, R Deiterding, Z Luan, F Xing, Y You
Combustion and Flame 198, 69-80, 2018
622018
Effects of transverse jet parameters on flame propagation and detonation transition in hydrogen–oxygen–argon mixture
H Peng, Y Huang, R Deiterding, Y You, Z Luan
Combustion Science and Technology 193 (9), 1516-1537, 2021
162021
A solver for simulating shock-induced combustion on curvilinear adaptive meshes
H Peng, CWC Atkins, R Deiterding
Computers & Fluids 232, 105188, 2022
52022
Study on Effects of Fluidic Obstacles on Flame Acceleration and Deflagration-to-Detonation Transition
C Liu, Y Huang, W Yang, H Peng, F Xing, Y You
21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017
22017
A three-dimensional solver for simulating detonation on curvilinear adaptive meshes
H Peng, R Deiterding
Computer Physics Communications 288, 108752, 2023
12023
A detailed chemistry solver on adaptive curvilinear meshes and its application to rotating detonation simulations
H Peng
University of Southampton, 2024
2024
Adaptive three-dimensional simulations of rotating detonation with cooling walls
H Peng, R Deiterding
2023
Parallel adaptive simulation of rotating detonation engines
H Peng, R Deiterding
Civil-Comp, 2023
2023
Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets
Z Luan, Y Huang, R Deiterding, H Peng, Y You
Shock Waves 32 (7), 617-632, 2022
2022
A three-dimensional solver for simulating reactive flow on curvilinear parallel adaptive meshes
H Peng, R Deiterding
2022
Simulations of ethylene-oxygen rotating detonation waves under different local equivalence ratio
H Peng, R Deiterding
2022
Simulations of shock-induced combustion using adaptive mesh refinement algorithm on mapped meshes
H Peng, CWC Atkins, R Deiterding
APS Division of Fluid Dynamics Meeting Abstracts, P04. 001, 2020
2020
Experimental study of effects of fluidic obstacle parameters on deflagration-to-detonation transition
P Han, H Yue, LIU Chen, X Fei, L Zhenye
Acta Aeronautica et Astronautica Sinica, 2018
2018
Performance of ultra-compact inter-turbine burner with different inlet mass flow splits
P Han, H Yue, X Fei, LIU Chen, LIN Zhi-wei
Journal of Aerospace Power, 2017
2017
A Physics Based Reactor Network Model of RQL Combustors
Q Shen, Y Huang, F Xing, H Peng, Z Lin
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Articles 1–15