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Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
Authors:  Tong FL(童福林);  Yu ZP(于长平);  Tang ZG(唐志共);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.;  Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(6937Kb)  |  Favorite  |  View/Download：465/165  |  Submit date：2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation  
Numerical investigation of characteristic frequency excited highly underexpanded jets 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:  Li XP;  Fan E;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(3588Kb)  |  Favorite  |  View/Download：468/149  |  Submit date：2017/07/24
Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls 期刊论文
JOURNAL OF TURBULENCE, 2017, 卷号: 18, 期号: 6, 页码: 569-588
Authors:  Tong, Fulin;  Tang, Zhigong;  Yu ZP(于长平);  Zhu, Xingkun;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing, Peoples R China.
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Shock Wave/turbulent Boundary Layer Interaction  Wall Temperature  Turbulence Structure  Shock Motion  Dynamic Mode Decomposition  
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.
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Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Midinfrared Absorption Measurements of Nitrous Oxide in Ammonium Dinitramide Monopropellant Thruster 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 5, 页码: 1496
Authors:  Ceng H(曾徽);  Li F(李飞);  Zhang SH(张少华);  Yu XL(余西龙);  Zhang W;  Yao ZP;  Li, F (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Yu, XL
View  |  Adobe PDF(1759Kb)  |  Favorite  |  View/Download：412/163  |  Submit date：2016/01/08
Joint-constraint model for large-eddy simulation of helical turbulence 期刊论文
PHYSICAL REVIEW E, 2014, 卷号: 89, 期号: 4, 页码: 43021
Authors:  Yu CP(于长平);  Xiao ZL;  Shi YP;  Chen SY;  Xiao, ZL (reprint author), Peking Univ, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China.
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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
Authors:  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.
View  |  Adobe PDF(2048Kb)  |  Favorite  |  View/Download：394/235  |  Submit date：2016/02/01
Direct Numerical Simulation  Compressible Turbulence  Coherent Structures  Turbulent Boundary-layer Flow