APPLICATION OF RADIAL-EQUILIBRIUM CONDITION TO AXIAL-FLOW TURBOMACHINE DESIGN INCLUDING CONSIDERATION OF CHANGE OF ENTROPY WITH RADIUS DOWNSTREAM OF BLADE ROW

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Document Details

Document Type
Technical Report
Publication Date
Apr 14, 1954
Accession Number
AD0028962

Entities

People

  • Charles C. Giamati
  • James E. Hatch
  • Robert J. Jackson

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aspect Ratio
  • Axial Flow
  • Boundary Layer
  • Coefficients
  • Compressors
  • Curvature
  • Engineering
  • Equations
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Geometry
  • Guide Vanes
  • Hydrodynamics
  • Radial Flow
  • Stagnation Pressure
  • Viscous Flow