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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：244/38  |  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：281/58  |  Submit date：2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
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：670/299  |  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：320/96  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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
Authors:  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.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download：366/93  |  Submit date：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
Authors:  Lin X;  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(828Kb)  |  Favorite  |  View/Download：825/253  |  Submit date：2013/01/18
Radiation Measurements  Shock Wave  Mars Re-entry  Rotational Temperature  Vibrational Temperature  Radiation Measurements  Cn  Entry  Tube  Mixtures  Model  
LES prediction of space-time correlations in turbulent shear flows 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 4, 页码: 993-998
Authors:  Guo L(郭力);  Li D(李栋);  Zhang X(张星);  He GW(何国威);  He, GW;  Chinese Acad Sci, LNM, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(422Kb)  |  Favorite  |  View/Download：836/254  |  Submit date：2013/01/18
Large-eddy Simulation  Subgrid Scale Model  Space-time Correlation  Turbulent Shear Flows  Large-eddy Simulation  Channel Flow  Backscatter  Velocity  Models  Field  
Characteristics of compressible flow of supercritical kerosene 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 1, 页码: 8-13
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Wang J(王晶);  Yu G(俞刚);  Li JG(李建国);  Fan, XJ;  Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(484Kb)  |  Favorite  |  View/Download：982/304  |  Submit date：2013/01/18
Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion