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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：386/137  |  提交时间：2016/01/08
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：432/92  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
Near continuum flows over a sphere 期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 111, 页码: 62-68
作者:  Cai CP;  Sun QH(孙泉华);  Cai, CP (reprint author), New Mexico State Univ, Dept Mech & Aerosp Engn, Jett Hall 110,MSC 3450, Las Cruces, NM 88003 USA.
浏览  |  Adobe PDF(889Kb)  |  收藏  |  浏览/下载：483/140  |  提交时间：2015/04/28
Flow Computation  Navier-stokes Equations  Slip Flows  
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.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载：763/239  |  提交时间：2015/06/12
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：477/173  |  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  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(590Kb)  |  收藏  |  浏览/下载：366/92  |  提交时间：2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets  
高超声速进气道再起动特性研究 学位论文
硕士论文，北京: 中国科学院研究生院, 2015
作者:  徐骁
Adobe PDF(3705Kb)  |  收藏  |  浏览/下载：463/9  |  提交时间：2015/08/28
Numerical Study of Shock/Boundary Layer Interaction of Chemically Reacting Flow in Shock Tube 期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 617-621
作者:  Chen S(陈松);  Sun QH(孙泉华)
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：249/96  |  提交时间：2016/08/25
Shock/boundary-layer Interaction  Nonequilibrium Chemical Reactions  Shock Tube Flow  Weno Scheme