A Zonal Approach to the Design of Finite Element Grids for 3-D Transonic Flows with Complex Geometries.

Abstract

A block-structured solution scheme is developed for the analysis of three-dimensional transonic flows. The scheme is based on the solution of potential flow equations for individual blocks representing part of the flow field. Based on a previously developed block-structured grid generation scheme, appropriate computational grids are generated for each of the blocks depending on the complexity of the local flow field. The equations are then solved to provide a solution of a large problem in terms of an assembly of smaller problems for each block. Numerical results illustrate the applicability of the method for a three-dimensional flow field around a wing profile (NACA0012). Different block structures are analyzed to demonstrate the robustness and the accuracy of the developed method. Finally a three-dimensional wing-body configuration is analyzed and the results are compared with previously obtained single block solutions. The method is expandable to the solution of Euler and Navier-Stokes equations. It is also suited to be executed in a parallel processing environment. Keywords: Finite Element Method; Transonic Flow, Three Dimensional Flow; Potential Flow.

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1985
Accession Number
ADA162168

Entities

People

  • Akin Ecer

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Equations
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Incompressible Flow
  • Navier Stokes Equations
  • Parallel Computing
  • Parallel Processing
  • Potential Flow
  • Subsonic Flow
  • Three Dimensional
  • Transonic Flow
  • Wing Body Configurations

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design