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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)  |  Favorite  |  View/Download：67/11  |  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)  |  Favorite  |  View/Download：76/9  |  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)  |  Favorite  |  View/Download：70/5  |  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)  |  Favorite  |  View/Download：251/41  |  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)  |  Favorite  |  View/Download：285/59  |  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)  |  Favorite  |  View/Download：427/76  |  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)
View  |  Adobe PDF(9586Kb)  |  Favorite  |  View/Download：679/301  |  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)
View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download：327/99  |  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)
View  |  Adobe PDF(1468Kb)  |  Favorite  |  View/Download：366/109  |  Submit date：2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
An efficient unstructured WENO method for supersonic reactive flows 期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
View  |  Adobe PDF(3673Kb)  |  Favorite  |  View/Download：434/105  |  Submit date：2018/10/30
Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction