High-Speed Wind-Tunnel Tests of an NACA 16-009 Airfoil Having a 32.9-Percent-Chord Flap with an Overhang 20.7 Percent of the Flap Chord

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1947
Accession Number
ADA801236

Entities

People

  • David B. Stevenson
  • Robert W. Byrne

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Airfoils
  • Boundary Layer
  • Boundary Layer Transition
  • Coefficients
  • Compressive Properties
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Three Dimensional
  • Trailing Edges
  • Turbulent Flow
  • Wind Tunnel Tests
  • Wind Tunnels