Wind-Tunnel Tests of a Blunt-Nose Aileron with Beveled Trailing Edge on an NACA 66(215)-216 Airfoil with Several Modifications of Aileron Nose and Adjacent Airfoil Contour

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1945
Accession Number
ADA801276

Entities

People

  • J. D. Bird

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Agreements
  • Air Flow
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Mach Number
  • Reynolds Number
  • Trailing Edges
  • Two Dimensional
  • Two Dimensional Flow
  • Wind Tunnel Tests
  • Wind Tunnels