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Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
作者:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(578Kb)  |  收藏  |  浏览/下载：474/130  |  提交时间：2016/03/21
Preventing numerical oscillations in the flux-split based finite difference method for compressible flows with discontinuities 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2015, 卷号: 300, 页码: 269-287
作者:  He ZW;  Zhang YS;  Li XL(李新亮);  Li L;  Tian BL;  Tian, BL (reprint author), Inst Appl Phys & Computat Math, Lab Computat Phys, Beijing 100094, Peoples R China.
浏览  |  Adobe PDF(1414Kb)  |  收藏  |  浏览/下载：481/157  |  提交时间：2016/01/08
Compressible Flows  Contact Discontinuity  Material Interface  Numerical Oscillations  Finite Difference Method  Flux Vector Splitting  Weno  
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.
浏览  |  Adobe PDF(4711Kb)  |  收藏  |  浏览/下载：296/129  |  提交时间：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
A Slope Constrained 4th Order Multi-Moment Finite Volume Method with WENO Limiter 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 18, 期号: 4, 页码: 901-930
作者:  Sun ZY;  Teng HH(滕宏辉);  Xiao F;  Xiao, F (reprint author), Tokyo Inst Technol, Dept Energy Sci, Midori Ku, 4259 Nagatsuta, Yokohama, Kanagawa 2268502, Japan.
浏览  |  Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：336/128  |  提交时间：2016/01/08
Multi-moment Finite Volume Method  Weno  Flux Reconstruction  Compressible Flow  Conservative Method  Oscillation-suppressing  
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.
浏览  |  Adobe PDF(3301Kb)  |  收藏  |  浏览/下载：368/96  |  提交时间：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
作者:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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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：444/124  |  提交时间：2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number  
Improvement of weighted compact scheme with multi-step strategy for supersonic compressible flow 期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 115, 页码: 2841-2849
作者:  Peng J(彭峻);  Shen YQ(申义庆);  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(3436Kb)  |  收藏  |  浏览/下载：383/137  |  提交时间：2016/01/08
Numerical Method  Supersonic Compressible Flow  Weighted Compact Scheme  Multi-step Strategy  
Reflection and transmission of elastic waves at the interface between two gradient-elastic solids with surface energy 期刊论文
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2015, 卷号: 52, 页码: 54-71
作者:  Li YQ;  Wei PJ;  Teng HH(滕宏辉);  Wei, PJ (reprint author), Univ Sci & Technol Beijing, Dept Appl Mech, Beijing 100083, Peoples R China.
浏览  |  Adobe PDF(6086Kb)  |  收藏  |  浏览/下载：585/145  |  提交时间：2015/06/12
Gradient Elasticity  Microstructure Effects  Surface Effects  
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
作者:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  收藏  |  浏览/下载：424/90  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer