DIFFUSION FACTOR FOR ESTIMATING LOSSES AND LIMITING BLADE LOADINGS IN AXIAL-FLOW-COMPRESSOR BLADE ELEMENTS

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Document Details

Document Type
Technical Report
Publication Date
Jun 08, 1953
Accession Number
AD0011178

Entities

People

  • Francis C. Schwenk
  • Robert L. Broderick
  • Seymour Lieblein

Organizations

  • National Advisory Committee for Aeronautics

Tags

DTIC Thesaurus Topics

  • Angle Of Incidence
  • Axial Flow
  • Axial Flow Compressor Blades
  • Axial Flow Compressors
  • Boundary Layer
  • Compressor Blades
  • Compressors
  • Diffusion
  • Fluid Dynamics
  • Fluid Mechanics
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Static Pressure
  • Three Dimensional
  • Turbulent Boundary Layer
  • Two Dimensional