REVIEW OF HIGH-PERFORMANCE AXIAL-FLOW-COMPRESSOR BLADE-ELEMENT THEORY

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Document Details

Document Type
Technical Report
Publication Date
Apr 06, 1954
Accession Number
AD0029122

Entities

People

  • Seymour Lieblein

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axial Flow
  • Axial Flow Compressor Blades
  • Axial Flow Compressors
  • Boundary Layer
  • Compressor Blades
  • Compressors
  • Diffusion
  • Experimental Data
  • Geometry
  • Guide Vanes
  • Inlet Guide Vanes
  • Mach Number
  • Plastic Explosives
  • Pressure Distribution
  • Reynolds Number
  • Three Dimensional
  • Two Dimensional