Inviscid Compressible Flow Past a Multi-Element Aerofoil,

Abstract

A conformal transformation method is used to generate an orthogonal curvilinear grid for two- and three-element configurations. The compressible potential flow equations are solved by finite difference methods. The solution could serve as a starting point for an iterative solution of the full viscous compressible flow case. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1984
Accession Number
ADP004055

Entities

People

  • A. Suddhoo
  • I. M. Hall

Organizations

  • University of Manchester

Tags

DTIC Thesaurus Topics

  • Airfoils
  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Compressible Flow
  • Dynamics
  • Equations
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • High Lift
  • Layers
  • Mechanics
  • Physics
  • Potential Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Phased Array Antenna Design.