A Discussion of the Application of the Prandtl-Glauert Method to Subsonic Compressible Flow over a Slender Body of Revolution

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1946
Accession Number
ADA801253

Entities

People

  • Lester Lees

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Bodies
  • Compressible Flow
  • Equations
  • Flow
  • Geometric Forms
  • Geometry
  • Mach Number
  • Mathematics
  • Revolutions
  • Slender Bodies
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnels