AERODYNAMIC CHARACTERISTICS AT HIGH AND LOW SUBSONIC MACH NUMBERS OF FOUR NACA 6-SERIES AIRFOIL SECTIONS AT ANGLES OF ATTACK FROM -2 TO 31

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Document Details

Document Type
Technical Report
Publication Date
Jun 05, 1953
Accession Number
AD0011173

Entities

People

  • Elmer A. Horton
  • Homer B. Wilson

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Airfoils
  • Coefficients
  • Dynamic Pressure
  • Free Stream
  • Helicopter Rotors
  • Leading Edges
  • Mach Number
  • Measurement
  • Research Facilities
  • Reynolds Number
  • Stagnation Pressure
  • Stagnation Temperature
  • Test Methods
  • Wind Tunnels