Wind-Tunnel Tests of Ailerons at Various Speeds. 3 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.35-Aileron-Chord Frise Balance on the NACA 23012 Airfoil

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1943
Accession Number
ADA801269

Entities

People

  • W. B. Kemp
  • W. Letko

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • High Angles
  • Low Drag
  • Low Drag Airfoils
  • Mach Number
  • Measurement
  • Oscillation
  • Pressure Distribution
  • Reynolds Number
  • Surfaces
  • Wind Tunnel Tests
  • Wind Tunnels