Effects of Mach Number Up to 0.34 and Reynolds Number Up to 8 x 10(exp 6) on the Maximum Lift Coefficient of a Wing of NACA 66-Series Airfoil Sections

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1950
Accession Number
ADA382138

Entities

People

  • G. C. Furlong
  • James E. Fitzpatrick

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Barometric Pressure
  • Boundary Layer
  • Boundary Layer Flow
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Incompressible Flow
  • Leading Edges
  • Mach Number
  • Measurement
  • Peak Values
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Static Pressure
  • Two Dimensional