Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65 sub (112) -111 Airfoil with 35-Percent-Chord Slotted Flap to Determine Optimum Flap Configuration at Reynolds Number of 2.4 Million

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1947
Accession Number
ADA801237

Entities

People

  • Stanley F. Racisz

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Flow
  • Air Force
  • Aircrafts
  • Airfoils
  • Aluminum Alloys
  • Coefficients
  • Deflection
  • High Lift
  • Leading Edges
  • Military Organizations
  • Reynolds Number
  • Slotted Flaps
  • Test Methods
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnels