期刊文献+

降落伞的流场特性研究 被引量:6

Investigation on the characteristics of parachute flow-field
下载PDF
导出
摘要 降落伞的流场特性直接关系到降落伞的气动力性能,一直以来是降落伞研究中的核心问题。本文采用计算流体动力学(CFD)方法对降落伞的流场进行数值模拟。通过采用不同的网格生成方法对降落伞的绕流流场进行研究,表明生成网格质量对流场计算精度有很大的影响。在一系列数值实验的基础上,证明采用多块贴体坐标的网格处理方法能够获得良好的网格质量,同时还具有易于寻找伞衣内外面压力,计算稳定性、可靠性高等优点。在此基础上,采用了七孔探针对降落伞绕流流场进行了测量,实验结果和计算结果吻合较好。 The flow-field characteristics around a parachute are heavy related to its aero-dynamical performance and its investigation is the key problem in the research of parachute. The flow-field of the parachute is simulated by computational fluid dynamics (CFD) in this paper and the differential mesh generation method is adopted. The mesh quality affects the numerical calculation results of parachute flow-field. Numerical results of the full of parachute shows that multiple block body-fitted grid generation method has a series of advantages such as good mesh quality, easy to obtain the pressure inside and outside of the canopy, the high calculation stability and reliability. The real flow-field characteristics are measured using seven-hole probe. The calculation result is good consistent with the experimental datum.
作者 余莉 明晓
出处 《空气动力学学报》 EI CSCD 北大核心 2007年第3期306-310,共5页 Acta Aerodynamica Sinica
基金 国家自然科学基金资助(项目编号10377006)
关键词 降落伞 流场 数值模拟 实验研究 parachute flow-field calculator simulation experimental investigation
  • 相关文献

参考文献7

二级参考文献24

  • 1李声远.解决流体一弹性体耦合动力学问题的一种迭代方法[J].振动工程学报,2000,13:512-516.
  • 2Baker MD, Mathias DL, Roth KR, et al. Numerical investigation of slat and compressibility effects for a high-lift wing. AIAA Paper 99-0538, 1999.
  • 3Mathias DL, Roth KR, Ross JC, et al. Navier-Stokes analysis of the flow about a flap edge. AIAA Paper 95-0185,1995.
  • 4Takallu MA, Laflin KR. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments.AIAA Paper 98-0701, 1998.
  • 5Coirier W J, Powell KG. An accuracy assessment of Cartesian-mesh approaches for euler equations. AIAA Paper 93-3335-CP, 1993.
  • 6Anderson WK. A grid generation and flow solution method for the Euler equations on unstructured grids. Journal of Computational Physics, 1994, 110(1): 23~38.
  • 7Melton JE, Berger M J, Aftosmis M J, et al. 3D application of a Cartesian grid euler method. AIAA Paper 95-0853,1995.
  • 8Stolcis L, Johnston LJ. Solution of the Euler equation on unstructrued grids for two-dimensional compressible flow.Aeronautical Journal, 1990, 94(936): 181~195.
  • 9Gaitonde AL. A dual-time method for the solution of the unsteady Euler equations. Aeronautical Journal, 1994,98(978): 283~291.
  • 10Arnone A, Liou MS, Povinelli LA. Integration of NavierStokes equations using dual time stepping and a multigrid method. AIAA Journal, 1995, 33(6): 985~990.

共引文献24

同被引文献43

引证文献6

二级引证文献10

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