中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共7条，第1-7条 帮助

限定条件                    
已选(0)清除 条数/页：   排序方式：
Midinfrared Absorption Measurements of Nitrous Oxide in Ammonium Dinitramide Monopropellant Thruster 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 5, 页码: 1496
作者:  Ceng H(曾徽);  Li F(李飞);  Zhang SH(张少华);  Yu XL(余西龙);  Zhang W;  Yao ZP;  Li, F (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Yu, XL
浏览  |  Adobe PDF(1759Kb)  |  收藏  |  浏览/下载：395/159  |  提交时间：2016/01/08
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：385/137  |  提交时间：2016/01/08
Numerical Method  Supersonic Compressible Flow  Weighted Compact Scheme  Multi-step Strategy  
Experimental study on convection heat transfer and air drag in sinter layer 期刊论文
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2015, 卷号: 22, 期号: 7, 页码: 2841-2848
作者:  Pan LS(潘利生);  Wei XL(魏小林);  Peng Y;  Shi XB;  Liu HL;  Pan, LS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1145Kb)  |  收藏  |  浏览/下载：413/76  |  提交时间：2015/10/21
Sinter Layer  Convection Heat Transfer  Pressure Drop  
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：755/238  |  提交时间：2015/06/12
Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy  
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation 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:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(728Kb)  |  收藏  |  浏览/下载：274/88  |  提交时间：2017/05/05
Comparative Studies  Flow Charac  Teristics  High Order Harmonics  High Resolution  Instability Modes  Near  Field Structure  Shock Structure  Under  Expanded Jets  
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：364/92  |  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  
Large Eddy Simulation with Sub-grid Stress Determined by Molecular Simulation and its Applications for Turbulent Channel Flows 期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 88-92
作者:  Ceng DD(曾丹丹);  Zhong FQ(仲峰泉);  Fan J(樊菁)
浏览  |  Adobe PDF(394Kb)  |  收藏  |  浏览/下载：249/50  |  提交时间：2016/08/25
Turbulent Channel Flow  Large Eddy Simulation  Molecular Statistics  Diffusive Information Preservation