The use of a Navier-Stokes analysis to predict the change in turbine efficiency resulting from changes in blade surface roughness or incidence flow angles is discussed. The results of a midspan Navier-Stokes analysis are combined with those from a quasi-three-dimensional flow analysis code to predict turbine performance. A quasi-three-dimensional flow analysis code was used to determine turbine performance over a range of incidence flow angles. This analysis was done for a number of incidence loss models. The change in loss due to changes in incidence flows computed from the Navier-Stokes analysis is compared with the results obtained using the empirical loss models. The Navier-Stokes analysis was also used to determine the effects of surface roughness using a mixing length turbulence model, which incorporated the roughness height. The validity of the approach used was verified by comparisons with experimental data for a turbine with both smooth and rough blades tested over a wide range of blade incidence flow angles.
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ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
May 24–27, 1993
Cincinnati, Ohio, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7891-0
PROCEEDINGS PAPER
Prediction of Surface Roughness and Incidence Effects on Turbine Performance
R. J. Boyle
R. J. Boyle
NASA Lewis Research Center, Cleveland, OH
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R. J. Boyle
NASA Lewis Research Center, Cleveland, OH
Paper No:
93-GT-280, V03BT16A036; 10 pages
Published Online:
February 25, 2015
Citation
Boyle, RJ. "Prediction of Surface Roughness and Incidence Effects on Turbine Performance." Proceedings of the ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. Volume 3B: General. Cincinnati, Ohio, USA. May 24–27, 1993. V03BT16A036. ASME. https://doi.org/10.1115/93-GT-280
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