INVESTIGATION OF TURBINES FOR DRIVING SUPERSONIC COMPRESSORS. 4. DESIGN AND PERFORMANCE OF SECOND CONFIGURATION INCLUDING STUDY OF THREE-DIMENSIONAL FLOW EFFECTS

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Document Details

Document Type
Technical Report
Publication Date
May 18, 1953
Accession Number
AD0010713

Entities

People

  • Harold J. Schum
  • Warner L. Stewart
  • Warren J. Whitney

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Air Cooled
  • Blades
  • Compressors
  • Cooling
  • Efficiency
  • Flow
  • Hydrodynamics
  • Mach Number
  • Mass Flow
  • Measurement
  • National Security
  • Static Pressure
  • Three Dimensional
  • Three Dimensional Flow
  • Trailing Edges
  • Turbines
  • Turbojet Engines

Technology Areas

  • Hypersonics