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 (2 g) of 0–10 μ Arizona road dust (ARD) is delivered to the impingement array at three different temperatures (290, 500, and 725 K) and at fixed pressure ratio. Deposition results are presented for operating pressures from 1 to 15 atm. 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 computational fluid dynamics (CFD) study identifies the additional role of Reynolds number in both the impingement hole losses and the shear layer thickness.
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October 2018
Research-Article
Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure
C. Sacco,
C. Sacco
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
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C. Bowen,
C. Bowen
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Search for other works by this author on:
R. Lundgreen,
R. Lundgreen
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
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J. P. Bons,
J. P. Bons
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
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J. Bailey
J. Bailey
GE Aviation,
Cincinnati, OH 45215
Cincinnati, OH 45215
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C. Sacco
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
C. Bowen
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
R. Lundgreen
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
J. P. Bons
Department of Mechanical and
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
Aerospace Engineering,
Ohio State University,
Columbus, OH 43235
E. Ruggiero
GE Aviation,
Cincinnati, OH 45215
Cincinnati, OH 45215
J. Allen
GE Aviation,
Cincinnati, OH 45215
Cincinnati, OH 45215
J. Bailey
GE Aviation,
Cincinnati, OH 45215
Cincinnati, OH 45215
Contributed by the Turbomachinery Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received August 23, 2017; final manuscript received September 23, 2017; published online July 5, 2018. Editor: David Wisler.
J. Eng. Gas Turbines Power. Oct 2018, 140(10): 102605 (12 pages)
Published Online: July 5, 2018
Article history
Received:
August 23, 2017
Revised:
September 23, 2017
Citation
Sacco, C., Bowen, C., Lundgreen, R., Bons, J. P., Ruggiero, E., Allen, J., and Bailey, J. (July 5, 2018). "Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure." ASME. J. Eng. Gas Turbines Power. October 2018; 140(10): 102605. https://doi.org/10.1115/1.4038550
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