Wind-Tunnel Investigation of an NACA 23012 Airfoil with a 30-Percent-Chord Maxwell Slat and with Trailing-Edge Flaps

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1941
Accession Number
ADB807243

Entities

People

  • J. G. Lowry
  • J. W. Mckee

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Airfoils
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • High Angles
  • High Lift
  • Leading Edges
  • Navy
  • Reynolds Number
  • Slotted Flaps
  • Split Flaps
  • Trailing Edges
  • Wind Tunnels