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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
作者:  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)  |  收藏  |  浏览/下载：51/4  |  提交时间：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
作者:  Hu GH(胡国豪);  Zhong FQ(仲峰泉);  Chen KT(陈科挺)
Adobe PDF(2013Kb)  |  收藏  |  浏览/下载：53/2  |  提交时间：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
作者:  Wang XY(王小永);  Hong QZ(洪启臻);  Hu Y(胡远);  Sun QH(孙泉华)
Adobe PDF(2067Kb)  |  收藏  |  浏览/下载：56/1  |  提交时间：2023/04/20
Nonequilibrium flow  Two temperature model  Quasi classical trajectory  Non Boltzmann effect  Vibration dissociation coupling effect  
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
作者:  Zhang, Yichen;  Xiang, Gaoxiang;  Tu, Qirong;  Wang, Qiu;  Wei, Haotian
Adobe PDF(1789Kb)  |  收藏  |  浏览/下载：144/6  |  提交时间：2023/02/20
Acetylene  Finite wedge  Oblique detonation  Initiation characteristics  Equivalence ratio  
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
作者:  Li X(李冼);  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉)
Adobe PDF(4562Kb)  |  收藏  |  浏览/下载：161/22  |  提交时间：2022/07/18
Dimple depth  Kerosene  Convective heat transfer  Turbulent flow  
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
作者:  Li X(李冼);  Zhong FQ(仲峰泉);  Xing YF(邢云绯)
Adobe PDF(5257Kb)  |  收藏  |  浏览/下载：213/51  |  提交时间：2022/07/18
Rib height  Kerosene  Heat transfer enhancement  Turbulent flow  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
作者:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  收藏  |  浏览/下载：225/34  |  提交时间：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
作者:  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)  |  收藏  |  浏览/下载：262/52  |  提交时间：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
作者:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  收藏  |  浏览/下载：396/63  |  提交时间：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
作者:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(2084Kb)  |  收藏  |  浏览/下载：350/80  |  提交时间：2020/07/06
Large-eddy simulation  Subgrid-scale model  Rotating turbulent channel flow  
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
作者:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(4075Kb)  |  收藏  |  浏览/下载：301/88  |  提交时间：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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
作者:  Yao W(姚卫)
浏览  |  Adobe PDF(9586Kb)  |  收藏  |  浏览/下载：652/294  |  提交时间：2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
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
作者:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1468Kb)  |  收藏  |  浏览/下载：340/100  |  提交时间：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
作者:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
浏览  |  Adobe PDF(3673Kb)  |  收藏  |  浏览/下载：402/97  |  提交时间：2018/10/30
Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction  
Influences of affiliated components and train length on the train wind 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
作者:  Guo DL(郭迪龙);  Shang KM;  Zhang Y;  Yang GW(杨国伟);  Sun ZX(孙振旭);  Guo, DL
浏览  |  Adobe PDF(10201Kb)  |  收藏  |  浏览/下载：291/121  |  提交时间：2017/09/04
Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 3, 页码: 362-368
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Yang Y;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuan Xi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1122Kb)  |  收藏  |  浏览/下载：366/93  |  提交时间：2016/09/14
3d Shock/shock Interaction  Mach Interaction  Spatial Dimension Reduction  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：334/84  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Direct Numerical Simulation of Compressible Turbulent Flows 期刊论文
ACTA MECHANICA SINICA, 2010, 卷号: 26, 期号: 6, 页码: 795-806
作者:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(2048Kb)  |  收藏  |  浏览/下载：386/231  |  提交时间：2016/02/01
Direct Numerical Simulation  Compressible Turbulence  Coherent Structures  Turbulent Boundary-layer Flow  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：298/96  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 4, 页码: 500-511
作者:  Wu CK(吴承康);  Pan WX(潘文霞);  Meng X(孟显);  Wang, Hai-Xing;  Wu, CK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(878Kb)  |  收藏  |  浏览/下载：454/127  |  提交时间：2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number