INVESTIGATION OF A TRANSLATING-CONE INLET AT MACH NUMBERS FROM 1.5 TO 2.0

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Document Details

Document Type
Technical Report
Publication Date
May 11, 1954
Accession Number
AD0030223

Entities

People

  • L. A. Leissler
  • William H. Sterbentz

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Diffusers
  • Drag
  • Dynamic Pressure
  • Engines
  • Flow
  • Free Stream
  • Geometry
  • Government Procurement
  • Jet Engines
  • Mach Number
  • Mass Flow
  • National Security
  • Shock
  • Static Pressure
  • Translations
  • Turbojet Engines