期刊文献+

二维非对称喷管数值模拟与验证 被引量:34

Simulation and Experiment Validation of a Two Dimensional Asymmetric Ramp Nozzle
下载PDF
导出
摘要 采用Fluent软件针对二维非对称喷管进行数值模拟,考察了其中几种常用湍流模型及网格密度对模拟精度的影响,并将计算结果与NASA公布的实验数据进行比较,找出了精度较高、求解快捷的模拟方案,结果表明FLUENT软件可以应用于带高超声速外流的非对称超声速喷管内外流场的数值计算。 The Computational fluid dynamics (CFD) software FLUENT was used to simulate the flow in the 2D asymmetric ramp-nozzle. The effect of four widely used turbulent models and three kinds of grid density on the numerical results were discussed. All the numerical results are compared with the experimental data published by NASA and agree with each other very well. It shows that FLUENT software with medium grid density and RNG k-Ε model can quickly yield accurate result, so it is very suitable for the internal and external flow simulation of a 2D asymmetric ramp nozzle with hypersonic free stream.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2004年第6期802-805,共4页 Journal of Aerospace Power
关键词 航空、航天推进系统 非对称大膨胀比喷管 高超声速 数值模拟 Fluent软件 Computational fluid dynamics Computer simulation Hypersonic flow Mathematical models Turbulent flow Two dimensional
  • 相关文献

参考文献3

  • 1Monta W J.Pitot Survey of Exhaust Flow Field of a 2-D Scramjet Nozzle with Air or Freon and Argon Used for Exhaust Simulation at Mach 6[R].NASA-TM-4361,1992.
  • 2Oktay Baysal.Flow Analysis and Design Optimization Methods for Nozzle Afterbody of a Hypersonic[R].NASA-CR-4431,1992.
  • 3FLUENT5 User's Guide[Z].1998,Vol.2.

同被引文献258

引证文献34

二级引证文献133

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部