Wind-Tunnel Tests of Ailerons at Various Speeds. 2 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.60 Aileron-Chord Sealed Internal 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
ADB803956

Entities

People

  • H. G. Denaci
  • J. D. Bird

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Airfoils
  • Airspeed
  • Boundary Layer
  • Coefficients
  • Control Surfaces
  • Deflection
  • Low Drag
  • Low Drag Airfoils
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Reynolds Number
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels