Coal ash deposition was numerically modeled on a GE-E3 high pressure turbine vane passage. A model was developed, in conjunction with FLUENT™ software, to track individual particles through the turbine passage. Two sticking models were used to predict the rates of deposition which were subsequently compared to experimental trends. The strengths and limitations of the two sticking models, the critical viscosity model and the critical velocity model, are discussed. The former model ties deposition exclusively to particle temperature while the latter considers both the particle temperature and velocity. Both incorporate some level of empiricism, though the critical viscosity model has the potential to be more readily adaptable to different ash compositions. Experimental results show that both numerical models are reasonably accurate in predicting the initial stages of deposition. Beyond the initial stage of deposition, for which transient effects must be accounted.
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January 2013
Research-Article
Coal Ash Deposition on Nozzle Guide Vanes—Part II: Computational Modeling
J. P. Bons
J. P. Bons
Department of Mechanical
and Aerospace Engineering
and Aerospace Engineering
Ohio State University
Columbus
, OH, 43235
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J. P. Bons
Department of Mechanical
and Aerospace Engineering
and Aerospace Engineering
Ohio State University
Columbus
, OH, 43235
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received July 15, 2011; final manuscript received August 16, 2011; published online November 6, 2012. Editor: David Wisler.
J. Turbomach. Jan 2013, 135(1): 011015 (9 pages)
Published Online: November 6, 2012
Article history
Received:
July 15, 2011
Revision Received:
August 16, 2011
Citation
Barker, B., Casaday, B., Shankara, P., Ameri, A., and Bons, J. P. (November 6, 2012). "Coal Ash Deposition on Nozzle Guide Vanes—Part II: Computational Modeling." ASME. J. Turbomach. January 2013; 135(1): 011015. https://doi.org/10.1115/1.4006399
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