Longitudinal Aerodynamic Characteristics of Five Hypersonic Missile Configurations at Mach Numbers from 2.01 to 6.01

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1961
Accession Number
AD0323074

Entities

People

  • George C. Ashby Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aeronautics
  • Afterbodies
  • Base Pressure
  • Bodies
  • Boundary Layer
  • Celestial Brightness
  • Fineness Ratio
  • Flared Afterbodies
  • Geometry
  • Government Procurement
  • Hypersonic Missiles
  • Leading Edges
  • Mach Number
  • Pressure Measurement
  • Reynolds Number

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow