An Analytical Study of Flow Losses through a Two-Dimensional Turbine Cascade with Boundary Layer Injection.

Abstract

A method for determining the performance of a two-dimensional turbine cascade with boundary layer injection is developed using existing incompressible boundary layer approximate solutions with a new formulation for the injection. The overall cascade loss includes friction and wake mixing losses. The results of the analysis are compared with experimentally obtained data as a check of the validity of the new analytical method. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1972
Accession Number
AD0744535

Entities

People

  • R. Earley
  • Widen Tabakoff

Organizations

  • University of Cincinnati

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Friction
  • Layers
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design