Nonaxisymmetric turbine end wall design: Part II -- Experimental validation
The Durham Linear Cascade has been redesigned with the nonaxisymmetric profiled end wall described in the first part of this paper, with the aim of reducing the effects of secondary flow. The design intent was to reduce the passage vortex strength and to produce a more uniform exit flow angle profile in the radial direction with less overturning at the wall. The new end wall has been tested in the linear cascade and a comprehensive set of measurements taken. These include traverses of the flow field at a number of axial planes and surface static pressure distributions on the end wall. Detailed comparisons have been made with the CFD design predictions, and also for the results with a planar end wall. In this way an improved understanding of the effects of end wall profiling has been obtained. The experimental results generally agree with the design predictions, showing a reduction in the strength of the secondary flow at the exit and a more uniform flow angle profile. In a turbine stage these effects would be expected to improve the performance of any downstream blade row. There is also a reduction in the overall loss, which was not given by the CFD design predictions. Areas where there are discrepancies between the CFD calculations and measurement are likely to be due to the turbulence model used. Conclusions for how the three-dimensional linear design system should be used to define end wall geometries for improved turbine performance are presented.
- Research Organization:
- Univ. of Durham (GB)
- OSTI ID:
- 20086928
- Journal Information:
- Journal of Turbomachinery, Vol. 122, Issue 2; Conference: 44th International Gas Turbine and Aeroengine Congress and Exhibition, Indianapolis, IN (US), 06/07/1999--06/10/1999; Other Information: PBD: Apr 2000; ISSN 0889-504X
- Country of Publication:
- United States
- Language:
- English
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