ANGLE-OF-ATTACK SUPERSONIC PERFORMANCE OF A CONFIGURATION CONSISTING OF A RAMP-TYPE SCOOP INLET LOCATED EITHER ON TOP OR BOTTOM OF A BODY OF REVOLUTION

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1954
Accession Number
AD0030360

Entities

People

  • Emil J. Kremzier
  • Robert C. Campbell

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Boundaries
  • Boundary Layer
  • Diffusers
  • Dynamic Pressure
  • Engines
  • Flow
  • Free Stream
  • Government Procurement
  • Jet Aircraft
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Measurement
  • Propulsion Systems
  • Static Pressure
  • Turbojet Engines

Technology Areas

  • Hypersonics