|
Selected(0)Clear
Items/Page: Sort: |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors: Yang L; 岳连捷 ; 张启帆; 张新宇
 Adobe PDF(1289Kb) |  Favorite | View/Download：215/53 | Submit date：2021/01/12 |
| 气相爆轰波DDT过程的物理模型 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors: 张文硕; 刘云峰; 姜宗林
Adobe PDF(1600Kb) | Favorite | View/Download：275/80 | Submit date：2019/11/21
气相爆轰 爆燃转爆轰 DDT 物理模型 |
| A microscopic study of one-dimensional H2-O2 detonation using DSMC method 会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
Authors: Yang C(杨超); Huang HJ(黄河激); Sun QH(孙泉华)
Adobe PDF(936Kb) | Favorite | View/Download：172/70 | Submit date：2020/11/20 |
| Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors: Wang Y; Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1120Kb) | Favorite | View/Download：502/109 | Submit date：2018/12/26 |
| A hybrid kinetic WENO scheme for compressible flow simulations 会议论文
The 10th International Conference on Computational Fluid Dynamics (ICCFD10), Barcelona,Spain, July 9-13, 2018
Authors: Liu HW(刘洪伟); Yu ZP(于长平); Li XL(李新亮)
Adobe PDF(878Kb) | Favorite | View/Download：410/82 | Submit date：2018/11/09
Gas Kinetic Theory Numerical Dissipation Weno Method Hybrid Numerical Flux High Order Schemes |
| 基于两步反应模型的斜爆轰波面不稳定性的数值研究 会议论文
中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23
Authors: 杨鹏飞; 滕宏辉; 姜宗林
Adobe PDF(893Kb) | Favorite | View/Download：310/60 | Submit date：2018/12/12
斜爆轰波 两步反应 波面不稳定性 |
| 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
Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1377Kb) | Favorite | View/Download：289/113 | Submit date：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| 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
Authors: Lee YC; Yao W(姚卫); Fan XJ(范学军); Yao, Wei(weiyao@imech.ac.cn)
Adobe PDF(1358Kb) | Favorite | View/Download：435/111 | Submit date：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
Authors: Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(623Kb) | Favorite | View/Download：271/94 | Submit date：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
 View |  Adobe PDF(1249Kb) | Favorite | View/Download：316/93 | Submit date：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
