Euromech 75 Lecture: Iterative Calculation of Subcritical Flow Around Thick Cambered Wings: Direct and Design Problems.

Abstract

This is a written version of a lecture given by the author at Euromech Colloquium 75 which was held at Rhode, near Braunschweig in May 1976. The subject of the colloquium was 'The calculation of flow fields by panel methods' and this paper describes iterative calculations of the classic problems of steady inviscid flow around a thick cambered wing, providing improved accuracy in relation to the so-called RAE Standard Method. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1977
Accession Number
ADA047019

Entities

People

  • C. C. L. Sells

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Boundaries
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Equations
  • Flow
  • Flow Fields
  • Incompressible Flow
  • Integral Equations
  • Inviscid Flow
  • Load Distribution
  • Mach Number
  • Pressure Distribution
  • Stratified Fluids
  • Swept Wings
  • Trailing Edges

Readers

  • Academic Conference Management
  • Aerodynamics/Aeronautics.
  • Linear Algebra