Computer Program for Calculation of Airfoil Pressure and Turbulent Friction Drag.

Abstract

A computer program has been developed which calculates approximate pressure drag coefficient values of thin symmetrical airfoil sections based on convex airfoil data. Flat plate turbulent friction results are also included for fully developed turbulent flow. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1977
Accession Number
ADA118388

Entities

People

  • Joseph J. Franz

Organizations

  • Naval Air Warfare Center Warminster

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Boundary Layer
  • Computer Programs
  • Computers
  • Drag
  • Fighter Aircraft
  • Flow
  • Fluid Dynamics
  • Free Stream
  • Friction
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Specific Heat
  • Turbulent Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.