Investigation of Aerodynamic Analysis Problems in Transonic Maneuvering. Volume II. Airfoil Analysis Computer Program.

Abstract

The report describes a computer program designed to facilitate the analysis of mono- and multi-element airfoils at subsonic flight conditions with attached flow. This program is a consolidation of several existing computer programs so that they are compatible, have standard interfaces, and operate together as one very large program. This program includes a potential flow analysis, supercritical pressure calculations, and boundary layer calculations using either a finite-difference method or an integral method. Application studies using this program are described in Volume 1 of this report. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0740124

Entities

People

  • Arvel E. Gentry

Organizations

  • Douglas

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Computer Programs
  • Computers
  • Flight
  • Flow
  • Integrals
  • Layers
  • Potential Flow
  • Subsonic Flight

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Fluid Dynamics.