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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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Control of shock-wave/boundary-layer interaction using abackward-facing step
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW(张伟为)
Adobe PDF(4533Kb)
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View/Download:177/44
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Submit date:2022/12/20
Shock-wave/boundary-layer interaction
Backward-facing step
Flow separation
Hypersonic inlet
Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 124, 页码: 17
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhuo, Changfei
;
Zhou, Shengbing
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(6822Kb)
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View/Download:185/32
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Submit date:2022/07/18
Hypervelocity double-wedge flow
High temperature non-equilibrium effects
Laminar and turbulence flow
Shock wave interaction
Shock wave
boundary layer interaction
Thermochemical non-equilibrium effects on hypersonic shock wave/turbulent boundary-layer interaction
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 192, 页码: 1-14
Authors:
Jiang, Hao
;
Liu, Jun
;
Luo, Shichao
;
Huang, Wei
;
Wang, Junyuan
;
Liu MK(刘美宽)
Adobe PDF(9113Kb)
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View/Download:246/41
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Submit date:2022/05/17
Hypersonic flow
Shock wave/turbulent boundary-layer interactions
Thermochemical non-equilibrium
Turbulence model
Theories and methods for designing hypersonic high-enthalpy flow nozzles
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2554Kb)
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View/Download:158/35
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Submit date:2022/06/10
Boundary layer correction
High-enthalpy flow
Hypersonic wind tunnel
Nozzle design
Real-gas effects