INVESTIGATION OF ROTATING-STALL LIMITS IN A SUPERSONIC TURBOFAN ENGINE

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1957
Accession Number
AD0144847

Entities

People

  • James F. Dugan Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axial Flow
  • Axial Flow Compressors
  • Carburetors
  • Compressors
  • Engine Components
  • Engines
  • Experimental Data
  • Gas Turbines
  • Guide Vanes
  • High Pressure
  • Inlet Guide Vanes
  • Jet Engines
  • Mach Number
  • Static Pressure
  • Turbine Components
  • Turbofan Engines
  • Turbojet Engines

Technology Areas

  • Hypersonics