Wind-Tunnel Investigation of Air Loads over a Double Slotted Flap on the NACA 65(216)-215, a = 0.8 Airfoil Section

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 09, 1947
Accession Number
ADA801099

Entities

People

  • Fioravante Visconti

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Flow
  • Airfoils
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Reynolds Number
  • Skin Friction
  • Slotted Flaps
  • Surfaces
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnels