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Guo-Yan Zhao
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Year
Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder
G Zhao, M Sun, J Wu, X Cui, H Wang
Aerospace Science and Technology 87, 190-206, 2019
682019
On shock sensors for hybrid compact/WENO schemes
GY Zhao, MB Sun, S Pirozzoli
Computers & Fluids 199, 104439, 2020
402020
Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma
R Feng, J Zhu, Z Wang, F Zhang, Y Ban, G Zhao, Y Tian, C Wang, ...
Combustion and Flame 237, 111843, 2022
362022
A general framework for the evaluation of shock-capturing schemes
G Zhao, M Sun, A Memmolo, S Pirozzoli
Journal of Computational Physics 376, 924-936, 2019
362019
Experimental investigations of cavity parameters leading to combustion oscillation in a supersonic crossflow
GY Zhao, MB Sun, XL Song, XP Li, HB Wang
Acta Astronautica 155, 255-263, 2019
242019
Effects of injection on flame flashback in supersonic crossflow
G Zhao, J Du, H Yang, T Tang, M Sun
Aerospace Science and Technology 120, 107226, 2022
212022
Investigation of combustion characteristics in a scramjet combustor using a modified flamelet model
G Zhao, M Sun, H Wang, H Ouyang
Acta Astronautica 148, 32-40, 2018
212018
Numerical dissipation control in an adaptive WCNS with a new smoothness indicator
G Zhao, M Sun, S Xie, H Wang
Applied Mathematics and Computation 330, 239-253, 2018
202018
An efficient adaptive central-upwind WENO-CU6 numerical scheme with a new sensor
GY Zhao, MB Sun, Y Mei, L Li, HB Wang, GX Li, Y Liu, YC Sun, CH Liang
Journal of Scientific Computing 81, 649-670, 2019
182019
Investigations of injection parameters on combustion oscillation in a supersonic crossflow
GY Zhao, MB Sun, YN Wang, XP Li, HB Wang
Acta Astronautica 152, 426-436, 2018
172018
A conceptual design of shock-eliminating clover combustor for large scale scramjet engine
M Sun, Y Zhao, G Zhao, Y Liu
Acta Astronautica 130, 34-42, 2017
172017
A flamelet model for supersonic non-premixed combustion with pressure variation
GY Zhao, MB Sun, JS Wu, HB Wang
Modern Physics Letters B 29 (21), 1550117, 2015
172015
Numerical investigation of the scale effects of the flame flashback phenomenon in scramjet combustors
G Zhao, J Du, M Liu, H Wang, M Sun
Aerospace Science and Technology 119, 107165, 2021
142021
Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
MA Guangwei, SUN Mingbo, Z Guoyan, C Liang, W Hongbo, YU Jiangfei
Chinese Journal of Aeronautics 36 (1), 216-230, 2023
132023
Efficient WENOCU4 scheme with three different adaptive switches
L Li, H Wang, G Zhao, M Sun, D Xiong, T Tang
Journal of Zhejiang University-SCIENCE A 21 (9), 695-720, 2020
132020
Effect of injection Mach number on penetration in a supersonic crossflow
GX Li, MB Sun, JF Yu, CH Liang, Y Liu, GY Zhao, YH Huang
AIAA Journal 58 (3), 1216-1226, 2020
132020
An efficient low-dissipation hybrid central/WENO scheme for compressible flows
L Li, HB Wang, GY Zhao, MB Sun, DP Xiong, T Tang
International Journal of Computational Fluid Dynamics 34 (10), 705-730, 2020
112020
Evaluation of flamelet/progress variable model for the applications in supersonic combustion using hybrid RANS/LES approach
T Tang, H Wang, M Sun, G Zhao, J Yu, Z Fan, Z Wang
Aerospace Science and Technology 126, 107633, 2022
102022
Numerical study of transverse jet mixing and combustion in a high-enthalpy supersonic crossflow with trace gases
T Tang, Z Wang, J Yu, Y Huang, M Sun, H Wang, G Zhao, Y Yang, ...
Physics of Fluids 35 (3), 2023
82023
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
M Liu, M Sun, G Zhao, Y Meng, Y Huang, G Ma, H Wang
Aerospace Science and Technology 130, 107904, 2022
82022
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Articles 1–20