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首页> 外文期刊>Journal of Aircraft >Deforming Grid Technique Applied to Unsteady Viscous Flow Simulation by a Fully Implicit Solver
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Deforming Grid Technique Applied to Unsteady Viscous Flow Simulation by a Fully Implicit Solver

机译:完全隐式求解器在非定常粘性流模拟中的变形网格技术

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The main objective of the present paper is to document the extension of a grid-movement approach to unsteady viscous flow simulations. The grid-deformation technique based on a modified TFI algorithm is employed to the grid displacements for the oscillating airfoil. This method can be seen as a perturbation method that is independent of the initial grid generation. The present work is intentionally placed into a multiblock framework although only a simple test case is performed. For each moving block, the grid deformation is determined by the TFI perturbations according to the displacement of the block boundaries. The advantages of using interpolated displacements are being fast and simple. Another important feature of the approach is that it allows the overall quality of the initial grid to be maintained. This method provides an efficient way of deforming the grid during an unsteady flow calculation. The current application mainly evaluates the deforming-grid technique for unsteady viscous flow simulation in multiblock grid system. The test results have shown that the deforming-grid technique is very effective and can be employed to the more general motions, for example, deforming airfoils. To demonstrate the performance of this method for the general multiblock case, the next work is to extend it to three-dimensional unsteady viscous flows about a complex multicomponent. configuration. This work is currently underway.
机译:本文的主要目的是证明网格移动方法扩展到非稳态粘性流模拟。基于改进的TFI算法的栅格变形技术被用于振荡翼型的栅格位移。该方法可以看作是一种与初始网格生成无关的摄动方法。尽管仅执行了一个简单的测试用例,但当前的工作有意放入了一个多块框架中。对于每个运动块,根据块边界的位移,由TFI扰动确定网格变形。使用内插位移的优点是快速简便。该方法的另一个重要特征是,它可以保持初始网格的整体质量。此方法提供了一种在不稳定流量计算期间使网格变形的有效方法。当前的应用主要评估变形网格技术用于多块网格系统中的非稳态粘性流模拟。测试结果表明,变形网格技术非常有效,可用于更普遍的运动,例如变形机翼。为了证明此方法在一般多块情况下的性能,下一步是将其扩展到围绕复杂多组分的三维非稳态粘性流。组态。这项工作目前正在进行中。

著录项

  • 来源
    《Journal of Aircraft》 |2005年第5期|p.1371-1374|共4页
  • 作者单位

    Northwestern Polytechnical University, Xi' an, 710072 Shaanxi, People's Republic of China;

  • 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 航空;
  • 关键词

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