Wind Tunnel Tests of Ailerons at Various Speeds. 5 - Pressure Distributions over the NACA 66,2-216 and NACA 23012 Airfoils with Various Balances on 0.20-Chord Ailerons

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1943
Accession Number
ADA800944

Entities

People

  • H. G. Denaci
  • W. Letko

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Buildings And Structures
  • Coefficients
  • Deflection
  • Flow
  • Free Stream
  • Leading Edges
  • Lepidoptera
  • Low Angles
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Skin Friction
  • Static Pressure
  • Wind Tunnel Tests
  • Wind Tunnels