Coordinate System Control: Adaptive Meshes,

Abstract

In the numerical solution of transient fluid flow problems, the flow variables are calculated at a finite number of aircraft. Typically, the points form ordered arrays which are joined together in some systematic way to form a computation mesh. On this mesh, the flow equations are approximated by finite differences, which are then marched in time. An algorithm which concentrates and disperses points automatically based on the numerical solution of the flow equations is described as adaptive. Here, an adaptive algorithm is derived from a minimum principle, and its application to transient flow problems in two dimensions is described. The major topics discussed are the variational formulation of a mesh generator with interior control, its use in adaptively rezoning a time-dependent problem, and the solution of the inverse problem to allow adaptive zoning of arbitrary initial meshes.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1982
Accession Number
ADP000976

Entities

People

  • J. U. Brackbill

Organizations

  • Los Alamos National Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Algorithms
  • Computations
  • Coordinate Systems
  • Demographic Cohorts
  • Differential Equations
  • Equations
  • Flow
  • Fluid Flow
  • Grids
  • Inverse Problems
  • Partial Differential Equations

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)