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Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Funding Organization：National Natural Science Foundation of China
Community：高温气体动力学国家重点实验室
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Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
Authors:
Guo SQ(郭帅旗)
;
Liu W(刘文)
;
Zhang CA(张陈安)
;
Liu Y(刘洋)
;
Wang FM(王发民)
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View/Download：32/0
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Submit date：2024/02/05
Hypersonic waverider
Aerodynamic model
Symbolic regression
Bluntness effect
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:
Peng J(彭俊)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Adobe PDF(2165Kb)
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View/Download：418/96
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Submit date：2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
