Calculated Performance Curves for Three Axial Flow Compressors with Low, Medium and High Stagger Blades

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1946
Accession Number
ADA800716

Entities

People

  • Marjorie Mettam

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Axial Flow
  • Axial Flow Compressors
  • Combustion
  • Combustion Chambers
  • Compressor Blades
  • Compressors
  • Efficiency
  • Engines
  • Flow
  • Gas Turbines
  • Government (Foreign)
  • Heat Engines
  • Heat Transfer Devices
  • Internal Combustion Engines
  • Mass Flow