THEORETICAL PRESSURE DISTRIBUTIONS FOR SOME SLENDER WING-BODY COMBINATIONS AT ZERO LIFT

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1956
Accession Number
AD0092431

Entities

People

  • Paul F. Byrd

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Complex Variables
  • Differential Equations
  • Flow
  • Free Stream
  • Government Procurement
  • Governments
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Slender Bodies
  • Subsonic Flow
  • Supersonic Flow
  • Swept Wings
  • Trailing Edges
  • Two Dimensional