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Language:英语
Funding Organization:National Key Research and Development Program of China
Document Type:期刊论文
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A computational method for the load spectra of large-scale structures with a data-driven learning algorithm
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 卷号: 66, 期号: 1, 页码: 141-154
Authors:
Chen XJ(陈贤佳)
;
Yuan, Zheng
;
Li, Qiang
;
Sun, ShouGuang
;
Wei YJ(魏宇杰)
Adobe PDF(2512Kb)
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View/Download:296/88
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Submit date:2023/02/09
load spectrum
computational mechanics
deep learning
data-driven modeling
gated recurrent unit neural network
Experimental study on the evolution of mode waves in laminar boundary layer on a large-scale flat plate
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 1, 页码: 16
Authors:
Liu MK(刘美宽)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(5472Kb)
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View/Download:273/43
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Submit date:2022/03/05
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:348/97
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
A Sufficient and Necessary Condition of the Existence of WENO-Like Linear Combination for Finite Difference Schemes
期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2021, 卷号: 29, 期号: 2, 页码: 534-570
Authors:
Kang J(康健)
;
Li XL(李新亮)
Adobe PDF(403Kb)
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Submit date:2021/03/03
Finite difference
WENO
sufficient and necessary condition
proof
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
On the ideal weights for WENO/WENO-like finite difference schemes for the first derivative, I
期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 7, 页码: 12
Authors:
Kang J(康健)
;
Li XL(李新亮)
Adobe PDF(584Kb)
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Submit date:2020/09/07
Finite difference
weighted essentially non-oscillatory
ideal weights
proof
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:278/84
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Submit date:2020/05/18
Hypersonic
turbulence control
numerical simulation
riblet plate
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner
期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Yuan XX
;
Yu ZP(于长平)
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Submit date:2020/04/07
Shock wave
Turbulent boundary layer
Unsteadiness
Expansion corner