PERFORMANCE OF SUPERSONIC RAMP-TYPE SIDE INLET WITH COMBINATIONS OF FUSELAGE AND INLET THROAT BOUNDARY-LAYER REMOVAL

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Document Details

Document Type
Technical Report
Publication Date
Apr 25, 1956
Accession Number
AD0091959

Entities

People

  • Robert C. Campbell

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Base Pressure
  • Bleed Systems
  • Boundaries
  • Boundary Layer
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Government Procurement
  • Law
  • Mach Number
  • Mass Flow
  • National Security
  • Pressure Measurement
  • Static Pressure
  • Supersonic Wind Tunnels
  • Turbojet Engines
  • Wind Tunnels

Technology Areas

  • Hypersonics