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Knowledge Management System of Institue of Mechanics, CAS
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Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels
期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
Authors:
Han GL(韩桂来)
;
Qi L(齐力)
;
Jiang ZL(姜宗林)
Adobe PDF(1715Kb)
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View/Download:287/46
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Submit date:2022/11/08
Heat flux
Measurement
Data processing
Error
Approximate solution
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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View/Download:297/71
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
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:352/98
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
Adobe PDF(4402Kb)
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Finite obstacle effect on the aerodynamic performance of a hovering wing
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 12
Authors:
Yin B(银波)
;
Yang GW(杨国伟)
;
Prapamonthon P
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Submit date:2020/03/11
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
Adobe PDF(2082Kb)
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View/Download:449/194
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Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty