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Effect of particle presence on the incompressible inviscid flow through a two dimensional compressor cascadeA computational model is developed for calculating the flow field, in the presence of solid particles, through a two-dimensional compressor cascade. Results show that the effect of solid particles on the flow field contributes to the bending of the streamlines toward the blade suction surface. It is determined that the difference in the pressure coefficient for particulate flow, with 165 micron diameter for the particles, is of the order of 3 percent over the air only flow. The change in the pressure coefficients is shown to be much larger for very small particles. It was found that the total pressure loss associated with the particulate flow is very high for very small particles as compared with large particles. The total pressure loss is also shown to be higher for accelerating flow than for decelerating flow. The total pressure loss is shown to be directly proportional to the particle concentration. It is concluded that significant reductions in performance can occur in a real multistage machine due to the changes in the pressure ratios, particularly if the suspended matter is small particles.
Document ID
19830066723
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Balan, C.
(Cincinnati Univ. OH, United States)
Tabakoff, W.
(Cincinnati, University Cincinnati, OH, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
ASME PAPER 83-GT-95
Accession Number
83A47941
Funding Number(s)
CONTRACT_GRANT: DAAG29-82-K-0029
CONTRACT_GRANT: NSG-3218
Distribution Limits
Public
Copyright
Other

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