An Analytical Study of Flow Losses through a Two-Dimensional Turbine Cascade with Boundary Layer Injection.
CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING
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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
- Fluid Mechanics
- Jet and Gas Turbine Engines