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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Simple shape model for normal shock trains in straight channels
期刊论文
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2025, 卷号: 39, 期号: 1, 页码: 16./通讯作者:Chen, Hao, Yue, Lianjie
Authors:
Yu FY(于方游)
;
Huang, Tinglong
;
Chen H(陈昊)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
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View/Download:390/0
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Submit date:2025/02/17
Shock train
Mathematical model
Shock reflection
Isolator
Ramjet engine
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188./通讯作者:Yue, Lianjie
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696./通讯作者:Xui, Rui
Authors:
Xue R(薛瑞)
;
Zheng X
;
Yue LJ(岳连捷)
;
Zhang SK
;
Weng C
Adobe PDF(3251Kb)
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Submit date:2020/07/06
Compressible boundary layer combustion
Skin-friction reduction
Shock train/flame interaction
Role of wall temperature on shock train in a rectangular isolator
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Lu HB
;
Wang D
;
Chen X
;
Yue LJ(岳连捷)
;
Ji, Feng (
[email protected]
)
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Adobe PDF(560Kb)
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Submit date:2017/05/05
Aero
Heating
Dual Mechanisms
On Flow
Shock Train
Specific Heat Ratio
Total Pressure
Total Temperatures
Wall Temperatures