AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 6.8 OF TWO HYPERSONIC MISSILE CONFIGURATIONS, ONE WITH LOW-ASPECT-RATIO CRUCIFORM FINS AND TRAILING-EDGE FLAPS AND ONE WITH A FLARED AFTERBODY AND ALL-MOVABLE CONTROLS

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Document Details

Document Type
Technical Report
Publication Date
Aug 04, 1958
Accession Number
AD0300229

Entities

People

  • Peter T. Bernot
  • Ross B. Robinson

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Afterbodies
  • Aspect Ratio
  • Base Pressure
  • Bodies
  • Control Surfaces
  • Drag
  • Dynamic Pressure
  • Flaps (Control Surfaces)
  • Flared Afterbodies
  • Governments
  • Hypersonic Missiles
  • Leading Edges
  • Mach Number
  • Trailing Edges
  • United States Government

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow