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Funding Organization：National Key Research and Development Program of China
Funding Project：National Key Research and Development Program of China[2016YFA0401200]
Community：高温气体动力学国家重点实验室
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Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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View/Download：346/97
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Submit date：2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
Study on turbulence drag reduction of riblet plate in hypersonic turbulent flows
期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 3, 页码: 11
Authors:
Zhou H(周浩)
;
Li XL(李新亮)
;
Yu ZP(于长平)
Adobe PDF(3698Kb)
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View/Download：276/84
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Submit date：2020/05/18
Hypersonic
turbulence control
numerical simulation
riblet plate
