EFFECTS OF INLET-AIR-FLOW DISTORTION ON STEADY-STATE ALTITUDE PERFORMANCE OF AN AXIAL-FLOW TURBOJET ENGINE

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 27, 1955
Accession Number
AD0071668

Entities

People

  • E. W. Conrad
  • John E. Mcaulay
  • Morgan P. Hanson

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Axial Flow
  • Compressor Blades
  • Compressors
  • Exhaust Nozzles
  • Frequency
  • Fuel Consumption
  • Guide Vanes
  • Inlet Guide Vanes
  • Instrumentation
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Static Pressure
  • Steady State
  • Temperature Gradients
  • Turbojet Engines