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Three-Component Breakdown of Spurious Drag in Computational Fluid Dynamics

机译:计算流体动力学中的杂散阻力的三成分分解

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摘要

A three-component phenomenological breakdown of spurious pressure drag in computational fluid dynamics is derived, following a far-field formulation. The study is purposely restricted to solutions to the Euler equations, in which the spurious drag, also extant in viscous simulations, can best be detected and analyzed. The matter of far-field spurious-drag elimination, which must indeed be handled differently in viscous flow and in inviscid flow, is outside its scope. Each of the three spurious components is produced through a different process. The first two components, already identified in the past, are of an irreversible thermodynamic nature. The first one is related to vorticity normal to the velocity, as it appears in Crocco's relation. The second one is concomitant with destruction of vorticity parallel to the velocity. The third component, of a reversible nature, is purely due to the effect of the far-field boundary condition. It exists in two-dimensional flow as well as in three- dimensional flow, in which it is shown that it must be negative, while positive in two dimensions.
机译:遵循远场公式,得出了计算流体动力学中的杂散压力阻力的三成分现象学分解。该研究有意地局限于Euler方程的解,其中可以最好地检测和分析在粘性模拟中也存在的杂散阻力。消除远场杂散阻力的问题超出了它的范围,在杂散流和粘滞流中必须进行不同的处理。这三个杂散分量中的每一个都是通过不同的过程产生的。过去已经确定的前两个成分具有不可逆的热力学性质。第一个与垂直于速度的涡度有关,正如它在Crocco关系中出现的那样。第二个伴随着平行于速度的涡旋破坏。具有可逆性质的第三部分纯粹是由于远场边界条件的影响。它以二维流和三维流形式存在,其中表明它必须为负,而在二维中为正。

著录项

  • 来源
    《Journal of Aircraft》 |2015年第4期|1336-1344|共9页
  • 作者

    Destarac Daniel;

  • 作者单位

    Off Natl Etud & Rech Aerosp, Appl Aerodynam Dept, F-92190 Meudon, France;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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