The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1948
Accession Number
ADA380944

Entities

People

  • Donald J. Graham

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Boundaries
  • Boundary Layer
  • Layers
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Shock
  • Shock Waves
  • Trailing Edges
  • Two Dimensional
  • Two Dimensional Flow
  • Wind Tunnels