A new model is proposed for predicting particle rebound and deposition in environments relevant to gas turbine engines. The model includes the following physical phenomena: elastic deformation, plastic deformation, adhesion, and shear removal. It also incorporates material property sensitivity to temperature and tangential-normal rebound velocity cross-dependencies observed in experiments. The model is well-suited for incorporation in computational fluid dynamics (CFD) simulations of complex gas turbine flows due to its algebraic (explicit) formulation. Model predictions are compared to coefficient of restitution data available in the open literature as well as deposition results from two different high-temperature turbine deposition facilities. While the model comparisons with experiments are in many cases promising, several key aspects of particle deposition remain elusive. The simple phenomenological nature of the model allows for parametric dependencies to be evaluated in a straightforward manner. It is hoped that this feature of the model will aid in identifying and resolving the remaining stubborn holdouts that prevent a universal model for particle deposition.
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August 2017
Research-Article
A Simple Physics-Based Model for Particle Rebound and Deposition in Turbomachinery
J. P. Bons,
J. P. Bons
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
e-mail: bons.2@osu.edu
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
e-mail: bons.2@osu.edu
Search for other works by this author on:
R. Prenter,
R. Prenter
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Search for other works by this author on:
S. Whitaker
S. Whitaker
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Search for other works by this author on:
J. P. Bons
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
e-mail: bons.2@osu.edu
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
e-mail: bons.2@osu.edu
R. Prenter
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
S. Whitaker
Aerospace Research Center,
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
Department of Mechanical and
Aerospace Engineering,
The Ohio State University,
Columbus, OH 43235
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received January 10, 2017; final manuscript received January 25, 2017; published online March 28, 2017. Editor: Kenneth Hall.
J. Turbomach. Aug 2017, 139(8): 081009 (12 pages)
Published Online: March 28, 2017
Article history
Received:
January 10, 2017
Revised:
January 25, 2017
Citation
Bons, J. P., Prenter, R., and Whitaker, S. (March 28, 2017). "A Simple Physics-Based Model for Particle Rebound and Deposition in Turbomachinery." ASME. J. Turbomach. August 2017; 139(8): 081009. https://doi.org/10.1115/1.4035921
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