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Indexed By:EI
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Date Issued:2022
Community:高温气体动力学国家重点实验室
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Direct numerical simulations of a turbulent channel flow developing over convergent-divergent riblets
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2022, 卷号: 98, 页码: 18
Authors:
Guo TB(郭同彪)
;
Fang, Jian
;
Zhong, Shan
;
Moulinec, Charles
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View/Download:153/46
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Submit date:2022/12/20
Convergent-divergent riblets
Direct numerical simulation
Large-scale secondary flow motion
Turbulent kinetic energy budget
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System
期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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View/Download:316/93
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Submit date:2022/11/14
Two-stage to orbit
Numerical simulation
Stage separation
Hypersonic flow
Aerodynamic interference
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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View/Download:325/86
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Effect of expansion on the wall heat flux in a supersonic turbulent boundary layer
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 21
Authors:
Tong FL(童福林)
;
Dong, Siwei
;
Duan JY(段俊亦)
;
Yuan, Xianxu
;
Li XL(李新亮)
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Submit date:2022/12/29
Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor
期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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Submit date:2021/10/29
Wall heat flux in a supersonic shock wave/turbulent boundary layer interaction
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 16
Authors:
Tong FL(童福林)
;
Yuan, Xianxu
;
Lai, Jiang
;
Duan JY(段俊亦)
;
Sun, Dong
;
Dong, Siwei
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Submit date:2022/07/18
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow
期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:
Wu ZJ(吴振杰)
;
Zhang QF(张启帆)
;
Zhang X(张旭)
;
Luo WH(罗苇航)
;
Gao ZB(高占彪)
;
Yue LJ(岳连捷)
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Submit date:2022/07/18
Contribution of flow topology to the kinetic energy flux in hypersonic turbulent boundary layer
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 4, 页码: 23
Authors:
Xu, Dehao
;
Wang, Jianchun
;
Yu ZP(于长平)
;
Li XL(李新亮)
;
Chen, Shiyi
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Submit date:2022/06/11
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene
期刊论文
FUEL, 2022, 卷号: 313, 页码: 13
Authors:
Shen, Wubingyi
;
Huang, Yue
;
Yao W(姚卫)
;
Liu, Hedong
;
You, Yancheng
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Submit date:2022/05/17
Improved delayed detached eddy simulation
Liquid kerosene
Skeletal reaction mechanism
Equivalence ratio
Cavity-based scramjet combustor
Supersonic combustion
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor
期刊论文
AIAA JOURNAL, 2022, 页码: 7
Authors:
Zhang X(张旭)
;
Zhang QF(张启帆)
;
Wu ZJ(吴振杰)
;
Yue LJ(岳连捷)
;
Gao ZB(高占彪)
;
Luo WH(罗苇航)
;
Chen H(陈昊)
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Submit date:2022/03/22