ESTIMATED AERODYNAMIC CHARACTERISTICS FOR DESIGN OF THE F-86E AIRPLANE

Abstract

This report is a compilation of aerodynamic data for design of the F-86E airplane. The aerodynamic coefficients presented herein are based on wind tunnel tests conducted in the North American Aerodynamics laboratory 7.75 x 11 foot low speed wind tunnel and in the high speed Southern California Cooperative Wind Tunnel. NACA experimental results are also utilized.

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Document Details

Document Type
Technical Report
Publication Date
Dec 26, 1950
Accession Number
AD0069271

Entities

People

  • F. T. Gardner
  • H. T. Downey

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Air Force
  • Aircrafts
  • Airfoils
  • Airplanes
  • Aspect Ratio
  • Fuel Tanks
  • Horizontal Stabilizers
  • International Airports
  • Mach Number
  • Pressure Distribution
  • Scale Models
  • Stabilization Systems
  • Trim Tabs
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Technical Research and Report Writing.