Parallel Unstructured Mesh Adaptation for Transient Moving Body and Aeropropulsive Applications

Abstract

Adaptive, unstructured grid methods, in which the mesh is allowed to deform, and grid quality subsequently restored through localized coarsening and refinement, offer the potential of a more rapid, straightforward approach to generalized moving body problems. Automation of this mesh movement and quality correction strategy requires a close coupling with the flow solution process. With parallel simulations now common, parallel coarsening and refinement methods for moving meshes are needed. In this work, parallel mesh adaptation strategies are developed to treat deforming, decomposed domains. Distortion of the moving mesh is assessed using a deformation matrix analysis. A two-pass approach is implemented in which cell migration shifts the interprocessor boundary, thereby accommodating coarsening and refinement of the interprocessor faces. The adapted grids are rebalanced among the processors using available techniques. Representative cases are presented to demonstrate the parallel approach and maintenance of cell quality for practical separation events.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2004
Accession Number
ADA464881

Entities

People

  • G. M. Feldman
  • N. Sinha
  • P. A. Cavallo

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Aircrafts
  • Astronautics
  • Boundaries
  • Cell Movement
  • Chemical Reactions
  • Computational Fluid Dynamics
  • Equations
  • Equations Of Motion
  • Flow
  • Fluid Dynamics
  • Mechanics
  • Pressure Distribution
  • Relative Motion
  • Steady State
  • Three Dimensional
  • Turbulent Flow

Readers

  • Computational Fluid Dynamics (CFD)
  • Image Processing and Computer Vision.