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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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Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:
Duan JY(段俊亦)
;
Tong FL(童福林)
;
Li XL(李新亮)
;
Liu HW(刘洪伟)
Adobe PDF(6039Kb)
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View/Download:131/10
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Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Lai, Jiang
;
Sun, Dong
;
Yuan, Xianxu
Adobe PDF(4757Kb)
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View/Download:53/2
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Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
Adobe PDF(1844Kb)
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Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
Effect of rib height on turbulent flow and heat transfer of kerosene in rectangular duct
期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 7, 页码: 12
Authors:
Li X(李冼)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
Adobe PDF(5257Kb)
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Submit date:2022/07/18
Rib height
Kerosene
Heat transfer enhancement
Turbulent flow
Effect of dimple depth on turbulent flow and heat transfer of kerosene in rectangular duct
期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 6, 页码: 12
Authors:
Li X(李冼)
;
Du MM(杜蒙蒙)
;
Zhong FQ(仲峰泉)
Adobe PDF(4562Kb)
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Submit date:2022/07/18
Dimple depth
Kerosene
Convective heat transfer
Turbulent flow
Oblique detonation wave triggered by a double wedge in hypersonic flow
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:
Teng, Honghui
;
Zhang, Yuhang
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(1747Kb)
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Submit date:2022/07/18
Double wedge
Hypersonic flow
Initiation structures
Oblique detonation
Shock interactions
Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2
期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors:
Shi Weixiu
;
Pan LS(潘利生)
;
Jin Suyi
;
Dong YH(董跃华)
;
Li T(李腾)
;
Zhao J(赵京)
;
Wei XL(魏小林)
Adobe PDF(2198Kb)
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Submit date:2021/11/01
CO2-based mixture
flammability
laminar flame speed
flammable critical mixing ratio
transcritical power cycle
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
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation