A DETAILED EXPERIMENTAL COMPARISON OF AXIAL COMPRESSOR BLADES DESIGNED FOR FREE VORTEX FLOW AND EQUIVALENT UNTWISTED AND TWISTED CONSTANT SECTION BLADES

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1953
Accession Number
AD0020208

Entities

People

  • Hannah M. Ogden
  • S. J. Andrews

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Angular Momentum
  • Bearings
  • Boundary Layer
  • Coefficients
  • Compressor Blades
  • Compressors
  • Diameters
  • Efficiency
  • Flow
  • Government Procurement
  • Governments
  • Mass Flow
  • Measurement
  • Reynolds Number
  • Static Pressure
  • Test Equipment