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Laminar flame speed of lignocellulosic biomass-derived oxygenates and blends of gasoline/oxygenates 期刊论文
FUEL, 2017, 卷号: 202, 页码: 572-582
作者:  Wu Y;  Rossow B;  Modica V;  Yu XL(余西龙);  Wu LL;  Grisch F;  Wu, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1848Kb)  |  收藏  |  浏览/下载：389/138  |  提交时间：2017/08/15
Laminar Flame Speed  Oxygenated Fuels  Gasoline  High Pressure And High Temperature  
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：276/112  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
作者:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1329Kb)  |  收藏  |  浏览/下载：563/112  |  提交时间：2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
High-Throughput Particle Manipulation Based on Hydrodynamic Effects in Microchannels 期刊论文
MICROMACHINES, 2017, 卷号: 8, 期号: 3
作者:  Liu C(刘超);  Hu GQ(胡国庆);  Hu, GQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing Key Lab Engn Construct & Mech, Beijing 100190, Peoples R China.;  Hu, GQ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(7127Kb)  |  收藏  |  浏览/下载：3251/2991  |  提交时间：2017/07/24
Particle Manipulation  Inertial Lift  Viscoelastic Effects  Microfluidics  Lab On a Chip  High Throughput  
Bending-induced extension in two-dimensional crystals 期刊论文
ACTA MECHANICA SINICA, 2017, 卷号: 33, 期号: 1, 页码: 71-76
作者:  Pan DX(潘斗星);  Li Y;  Wang ZQ(王自强);  Guo WL;  Wang, TC (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1809Kb)  |  收藏  |  浏览/下载：303/94  |  提交时间：2017/04/26
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
浏览  |  Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：417/104  |  提交时间：2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：254/85  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
可压缩流动中间断问题的高分辨率数值求解方法及应用 学位论文
博士论文，北京: 中国科学院大学, 2017
作者:  刘利
Adobe PDF(16708Kb)  |  收藏  |  浏览/下载：352/12  |  提交时间：2019/05/15
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：477/90  |  提交时间：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：269/80  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion