DATA FROM LARGE-SCALE LOW-SPEED TESTS OF AIRPLANE CONFIGURATIONS WITH A THIN 45 SWEPT WING INCORPORATING SEVERAL LEADING-EDGE CONTOUR MODIFICATIONS

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Document Details

Document Type
Technical Report
Publication Date
May 07, 1956
Accession Number
AD0094326

Entities

People

  • William T. Evans

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Dynamic Pressure
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Leading Edge Flaps
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Split Flaps
  • Swept Wings
  • Wind Tunnels
  • Wing Tips