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APPROXIMATE THEORY FOR THE NONLINEAR EVOLUTION OF VORTEX SHEETS.

机译:涡旋片的非线性演化的近似理论。

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摘要

We study the nonlinear evolution of vortex sheet problems and formation of singularities, mainly: the flat 2-d vortex sheet perturbed initially by a small analytic disturbance, the circular vortex sheet, and the ring wing problem or nacelle. For the first, by a formal perturbation analysis, Moore derived an approximate differential equation for the evolution of the vortex sheet and used it to formally show that a sinusoidal perturbation of the flat vortex sheet develops a singularity at time t(,c) = 2(VBAR)log (epsilon)(VBAR) + 0(log(VBAR)log (epsilon)(VBAR)). We present a simplified derivation of Moore's approximate equation and the equivalent conservation law and show short time existence using Lax's a priori estimate theory for 2 x 2 systems of nonlinear conservation law. We also present a valid asymptotic expansion for a singular solution of Moore's equation and evaluate Birkhoff's singular integral in some interesting cases that give information about the validity of Moore's approximate equation, type of singularity and motion of singularities. For the circular vortex sheet we present its linear theory and propose an approximate system of equations to study its nonlinear evolution. Finally, for the ring wing or nacelle problem we present a Moore's type of equation to study its nonlinear evolution.
机译:我们研究了涡旋片问题的非线性演化和奇点的形成,主要是:平面二维涡旋片最初受到较小的解析扰动扰动,圆形涡旋片以及环形翼问题或机舱。首先,通过形式化扰动分析,Moore推导了涡旋片演化的近似微分方程,并用它正式表明平坦涡旋片的正弦扰动在时间t(,c)= 2时产生奇异性(VBAR)log(ε)(VBAR)+ 0(log(VBAR)log(epsilon)(VBAR)))。我们给出了Moore近似方程和等效守恒律的简化推导,并显示了使用Lax的2x 2非线性守恒律系统的先验估计理论存在的短时间。我们还给出了Moore方程奇异解的有效渐近展开,并在一些有趣的情况下评估Birkhoff奇异积分,这些信息提供了有关Moore近似方程有效性,奇异类型和奇异运动的信息。对于圆形涡旋片,我们介绍了其线性理论并提出了近似的方程组来研究其非线性演化。最后,对于环形翼或机舱问题,我们提出了一种摩尔类型的方程,以研究其非线性演化。

著录项

  • 作者

    ORELLANA, OSCAR.;

  • 作者单位

    New York University.;

  • 授予单位 New York University.;
  • 学科 Mathematics.
  • 学位 Ph.D.
  • 年度 1987
  • 页码 106 p.
  • 总页数 106
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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