Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine. 7 - Pressure and Temperature Distributions

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Document Details

Document Type
Technical Report
Publication Date
Dec 10, 1948
Accession Number
ADA801169

Entities

People

  • Martin J. Saari
  • William R. Prince

Organizations

  • National Advisory Committee for Aeronautics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Axial Flow
  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Exhaust Nozzles
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Sea Level
  • Static Pressure
  • Turbine Blades
  • Turbojet Engines
  • Wind Tunnels