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Evaluation of centrifugal compressor performance with water injectionThe effects of water injection on a compressor are presented. To determine the effects of varying water-air ratio, the compressor was operated at a constant equivalent impeller speed over a range of water-air ratios and weight flows. Operation over a range of weight flows at one water-air ratio and two inlet air temperatures was carried out to obtain an indication of the effects of varying inlet air temperature. Beyond a water-air ratio of 0.03 there was no increase in maximum air-weight flow, a negligible rise in peak total-pressure ratio, and a decrease in peak adiabatic efficiency. An increase in inlet air temperature resulted in an increase in the magnitude of evaporation. An analysis of data indicated that the magnitude of evaporation within the compressor impeller was small.
Document ID
19930086705
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Beede, William L
Hamrick, Joseph T
Withee, Joseph R , Jr
Date Acquired
August 16, 2013
Publication Date
July 18, 1951
Report/Patent Number
NACA-RM-E51E21
Report Number: NACA-RM-E51E21
Accession Number
93R15995
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPRESSORS - RADIAL FLOW
TURBINES, GAS - LIQUID INJECTION
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