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仲峰泉 [7]
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Indexed By:CSCD
Source Publication:ACTA MECHANICA SINICA
Community:高温气体动力学国家重点实验室
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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences
期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:
Lin MY(林明月)
;
Yang F(杨帆)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
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View/Download:24/0
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Submit date:2024/05/27
Shock waves
Shock-shock interaction
Theoretical analysis
Hysteresis
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
An analytical model for maximum temperature and temperature distribution of plate structure with active cooling
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 5, 页码: 322290
Authors:
Hu GH(胡国豪)
;
Zhong FQ(仲峰泉)
;
Chen KT(陈科挺)
Adobe PDF(2013Kb)
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View/Download:73/8
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Submit date:2023/04/20
Plate structure
Active cooling
Thermal protection
Convective heat transfer
Analytical model
On the accuracy of two temperature models for hypersonic nonequilibrium flow
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 2, 页码: 122193
Authors:
Wang XY(王小永)
;
Hong QZ(洪启臻)
;
Hu Y(胡远)
;
Sun QH(孙泉华)
Adobe PDF(2067Kb)
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Submit date:2023/04/20
Nonequilibrium flow
Two temperature model
Quasi classical trajectory
Non Boltzmann effect
Vibration dissociation coupling effect
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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View/Download:254/62
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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
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
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
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
Adobe PDF(3790Kb)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows
期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Yu ZP(于长平)
Adobe PDF(2084Kb)
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Submit date:2020/07/06
Large-eddy simulation
Subgrid-scale model
Rotating turbulent channel flow