AERODYNAMICS OF SLENDER BODIES AT MACH NUMBER OF 3.12 AND REYNOLDS NUMBERS FROM 2X106 TO 15X106. V - AERODYNAMIC LOAD DISTRIBUTIONS FOR A SERIES OF FOUR BOATTAILED BODIES

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Document Details

Document Type
Technical Report
Publication Date
May 06, 1954
Accession Number
AD0030121

Entities

People

  • Barry Moskowitz
  • John R. Jack

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Base Pressure
  • Bodies Of Revolution
  • Boundary Layer
  • Cross Flow
  • Drag
  • Fineness Ratio
  • Free Stream
  • Geometry
  • Load Distribution
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Skin Friction
  • Slender Bodies
  • Static Pressure
  • Two Dimensional