Accession Number:
AD0744535
Title:
An Analytical Study of Flow Losses through a Two-Dimensional Turbine Cascade with Boundary Layer Injection.
Descriptive Note:
Technical rept.,
Corporate Author:
CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING
Personal Author(s):
Report Date:
1972-04-01
Pagination or Media Count:
52.0
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
Descriptors:
Subject Categories:
- Fluid Mechanics
- Jet and Gas Turbine Engines