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Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 1, 页码: 131-140
Authors:  Zhu XK;  Yu ZP(于长平);  Tong FL;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Preventing numerical oscillations in the flux-split based finite difference method for compressible flows with discontinuities, II 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2016, 卷号: 80, 期号: 5, 页码: 306-316
Authors:  He ZW;  Zhang YS;  Li XL(李新亮);  Tian BL;  Tian, BL (reprint author), Inst Appl Phys & Computat Math, Beijing 100094, Peoples R China.
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Contact Discontinuity  Material Interface  Finite Difference Method  Flux Vector Splitting  Local Characteristic Decomposition  Equation Of State  Weno  
Nonlinear spectral-like schemes for hybrid schemes 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2014, 卷号: 57, 期号: 4, 页码: 753-763
Authors:  He, ZW;  Li XL(李新亮);  Liang X(梁贤);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Group Velocity Control  Hybrid  Weno  Shockwave-turbulent Boundary Layer Interaction  Direct Numerical Simulation  
Optimized sixth-order monotonicity-preserving scheme by nonlinear spectral analysis 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2013, 卷号: 73, 期号: 6, 页码: 560–577
Authors:  Li XL(李新亮);  Leng Y(冷岩);  He ZW(何志伟);  Li, XL (reprint author), Chinese Acad Sci, LHD Inst Mech, Beijing 100190, Peoples R China
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Nonlinear Spectral Analysis  Monotonicity-preserving  Optimization  Shock-capturing Schemes  Dissipation  Dispersion  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
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Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models  
A 5th order monotonicity-preserving upwind compact difference scheme 期刊论文
Science China, Physics, Mechanics & Astronomy, 2011, 卷号: 54, 期号: 3, 页码: 511-522
Authors:  He ZW(何志伟);  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Li, XL (reprint author), Chinese Acad Sci, Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China
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Upwind Compact Scheme  Monotonicity-preserving  Compressible Flows  Shock Capturing Scheme  Hyperbolic Conservation-laws  Essentially Nonoscillatory Schemes  Shock-turbulence Interaction  High-resolution Schemes  High-order  Efficient Implementation  Flow