Wind-Tunnel Tests of Ailerons at Various Speeds. 1 - Ailerons of 0.20 Airfoil Chord and Tube Contour with 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1943
Accession Number
ADB807290

Entities

People

  • C. Freed
  • H. G. Denaci
  • W. Letko

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Airfoils
  • Boundary Layer
  • Coefficients
  • Deflection
  • Fluid Mechanics
  • Low Drag
  • Low Drag Airfoils
  • Mach Number
  • Measurement
  • Mechanics
  • Pressure Distribution
  • Reynolds Number
  • Surfaces
  • Wind Tunnel Tests
  • Wind Tunnels