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An airplane jig shape design method based on high fidelity aeroelastic simulation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
作者:  Yang W;  Wang QF;  Zhou L;  Zheng GN(郑冠男);  Liu W;  Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Aeroelasticity  Cfd  Csd  Jig Shape  Structural Mesh  
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.
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Compressible Flows  Contact Discontinuity  Material Interface  Numerical Oscillations  Finite Difference Method  Flux Vector Splitting  Weno  
Dissipative Particle Dynamics (DPD): An Overview and Recent Developments 期刊论文
ARCHIVES OF COMPUTATIONAL METHODS IN ENGINEERING, 2015, 卷号: 22, 期号: 4, 页码: 529-556
作者:  Liu MB(刘谋斌);  Liu GR;  Zhou LW;  Chang JZ;  Liu, MB (reprint author), Chinese Acad Sci, Inst Mech, 15 Bei Si Huan Xi Rd, Beijing 100190, Peoples R China.
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Dissipative Particle Dynamics (Dpd)  Meshfree Method  Particle Method  Coarse-grained Method  Mesoscale  Multiscale  
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  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
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.
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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.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
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.
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Numerical Method  Supersonic Compressible Flow  Weighted Compact Scheme  Multi-step Strategy  
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:426/91  |  提交时间:2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
Experimental study on spectrum and multi-scale nature of wall pressure and velocity in turbulent boundary layer 期刊论文
CHINESE PHYSICS B, 2015, 卷号: 24, 期号: 6, 页码: 64702
作者:  Zheng Xiao-Bo;  Jiang Nan;  Jiang, N (reprint author), Tianjin Univ, Dept Mech, Tianjin 300072, Peoples R China.
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Multi-scale Coherent Structures  Hot Wire Anemometry  Microphone  Wavelet Transform