EFFECTS OF LEADING-EDGE RADIUS AND MAXIMUM THICKNESS-CHORD RATIO ON THE VARIATION WITH MACH NUMBER OF THE AERODYNAMIC CHARACTERISTICS OF SEVERAL THIN NACA AIR-FOIL SECTIONS

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Document Details

Document Type
Technical Report
Publication Date
Apr 14, 1954
Accession Number
AD0029128

Entities

People

  • Donald J. Graham
  • Robert E. Berggren

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aluminum Alloys
  • Coefficients
  • Free Stream
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Reynolds Number
  • Rubber Gaskets
  • Thickness
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels