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Harmonic growth of spherical Rayleigh-Taylor instability in weakly nonlinear regime 期刊论文
PHYSICS OF PLASMAS, 2015, 卷号: 22, 期号: 11, 页码: 112112
作者:  Liu WH(刘万海);  Chen YL;  Yu ZP(于长平);  Li XL(李新亮)
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A hybrid kinetic WENO scheme for inviscid and viscous flows 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2015, 卷号: 79, 期号: 6, 页码: 290-305
作者:  Liu HW(刘洪伟)
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Weno Schemes  Kinetic Numerical Fluxes  Numerical Dissipations  
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
作者:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Experimental Study of the Transient Response of Bunsen Flame to Nanosecond Pulsed Discharges 期刊论文
PLASMA CHEMISTRY AND PLASMA PROCESSING, 2015, 卷号: 35, 期号: 6, 页码: 1029-1042
作者:  Zhang SH(张少华);  Yu XL(余西龙);  Xiong H(熊恒);  Ceng H(曾徽);  Li F(李飞);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Nanosecond Pulsed Discharges (Npd)  Time-resolved Optical Emission Spectroscopy  Schlieren  
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
作者:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
A characteristic space-time conservation element and solution element method for conservation laws 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2015, 卷号: 288, 页码: 101-118
作者:  Shen H;  Wen CY;  Zhang DL(张德良);  Wen, CY (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
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Space-time Conservation Element And  Solution Element (Ce/se) Method  Upwind Scheme  Characteristic-based Scheme  Riemann Solver  
Robust high-order space-time conservative schemes for solving conservation laws on hybrid meshes 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2015, 卷号: 281, 页码: 375-402
作者:  Shen H;  Wen CY;  Liu KX;  Zhang DL(张德良);  Shen, H (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
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Space-time Conservation Element And Solution Element (Ce/se) Method  High-order Accuracy  Hybrid Meshes  Unstructured Meshes  
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
作者:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
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Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
作者:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载:479/174  |  提交时间:2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients