The role of absolute pressure in deposition testing is reviewed from first principles. Relevant dimensionless parameters for deposition testing are developed and dynamic similarity conditions are assessed in detail. Criteria for establishing appropriate conditions for laboratory studies of deposition are established pursuant to the similarity variables. The role of pressure is particularly singled out for consideration relative to other variables such as temperature, particle size, and test article geometry/scaling. A case study is presented for deposition in a generic array of impinging jets. A fixed quantity (2g) of 0–10micron Arizona Road Dust (ARD) is delivered to the impingement array at three different temperatures (290, 500, and 725K) and at fixed pressure ratio. Deposition results are presented for operating pressures from 1 to 15atm. Surface scans show that the height of deposit cones at the impingement sites decreases with increasing pressure at constant temperature and pressure ratio. This reduction is explained by the lower “effective” Stokes number that occurs at high particle Reynolds numbers, yielding fewer particle impacts at high pressure. A companion CFD study identifies the additional role of Reynolds number in both the impingement hole losses as well as the shear layer thickness.
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ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
June 26–30, 2017
Charlotte, North Carolina, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5081-7
PROCEEDINGS PAPER
Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure
R. Lundgreen,
R. Lundgreen
Ohio State University, Columbus, OH
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J. P. Bons,
J. P. Bons
Ohio State University, Columbus, OH
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J. Bailey
J. Bailey
GE Aviation, Cincinnati, OH
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C. Sacco
Ohio State University, Columbus, OH
C. Bowen
Ohio State University, Columbus, OH
R. Lundgreen
Ohio State University, Columbus, OH
J. P. Bons
Ohio State University, Columbus, OH
E. Ruggiero
GE Aviation, Cincinnati, OH
J. Allen
GE Aviation, Cincinnati, OH
J. Bailey
GE Aviation, Cincinnati, OH
Paper No:
GT2017-64961, V02DT48A021; 15 pages
Published Online:
August 17, 2017
Citation
Sacco, C, Bowen, C, Lundgreen, R, Bons, JP, Ruggiero, E, Allen, J, & Bailey, J. "Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure." Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. Volume 2D: Turbomachinery. Charlotte, North Carolina, USA. June 26–30, 2017. V02DT48A021. ASME. https://doi.org/10.1115/GT2017-64961
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