Wind-Tunnel Tests of Ailerons at Various Speeds. 4 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-Chord Extreme Blunt-Nose Balance on the NACA 23012 Airfoil

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1943
Accession Number
ADA801268

Entities

People

  • R. A. Anderson
  • T. A. Hollingworth
  • W. Letko

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Airspeed
  • Boundary Layer
  • Coefficients
  • Compressive Properties
  • Deflection
  • Low Angles
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels