The Effect of Blade Lean on an Axial Turbine Stator Flow Having Various Hub Tip Ratios

Abstract

The effect of simple lean on an axial turbine stator was examined using a three dimensional viscous flow code. A constant section stator with no meridional contouring was chosen to isolate the effect of the lean. Four different lean angles were examined at three hub/tip ratios.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2002
Accession Number
ADA408925

Entities

People

  • Edward M. Bennet

Tags

DTIC Thesaurus Topics

  • Computational Fluid Dynamics
  • Computational Science
  • Equations
  • Flow
  • Flow Fields
  • Mach Number
  • Mass
  • Mass Flow
  • Navier Stokes Equations
  • New York
  • Pressure Gradients
  • Stators
  • Three Dimensional
  • Turbine Stators
  • Turbines
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.