Two-Dimensional Wind-Tunnel Investigation of the NACA 64 sub 1 -012 Airfoil Equipped with Two Types of Leading-Edge Flap

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1947
Accession Number
ADA800952

Entities

People

  • Felicien F. Fullmer Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Coefficients
  • Deflection
  • Geometry
  • High Lift
  • High Lift Devices
  • Leading Edge Flaps
  • Leading Edges
  • Measuring Instruments
  • Pressure Distribution
  • Roughness
  • Split Flaps
  • Surfaces
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnels