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Source Publication:ACTA MECHANICA SINICA
Language:英语
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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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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Submit date:2023/04/20
Plate structure
Active cooling
Thermal protection
Convective heat transfer
Analytical model
The initiation characteristics of oblique detonation in acetylene-air mixtures in the finite wedge
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 3, 页码: 9
Authors:
Zhang, Yichen
;
Xiang, Gaoxiang
;
Tu, Qirong
;
Wang, Qiu
;
Wei, Haotian
Adobe PDF(1789Kb)
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Submit date:2023/02/20
Acetylene
Finite wedge
Oblique detonation
Initiation characteristics
Equivalence ratio
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
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
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:
Yao W(姚卫)
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View/Download:670/299
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Submit date:2019/12/17
Kerosene
Supersonic combustion
Large eddy simulation
Skeletal mechanism
Scramjet
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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View/Download:320/96
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Adobe PDF(1468Kb)
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View/Download:360/107
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel