Evaluation of Centrifugal Compressor Performance With Water Injection

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Description

The 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 … continued below

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14 p.

Creation Information

Beede, William L.; Hamrick, Joseph T. & Withee, Joseph R., Jr. July 18, 1951.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 270 times. More information about this report can be viewed below.

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Description

The 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.

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14 p.

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  • Accession or Local Control No: 93R15995
  • URL: http://hdl.handle.net/2060/19930086705 External Link
  • Report No.: NACA-RM-E51E21
  • Center for AeroSpace Information Number: 19930086705
  • Archival Resource Key: ark:/67531/metadc58894

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

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Creation Date

  • July 18, 1951

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

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  • July 24, 2018, 3:56 p.m.

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Beede, William L.; Hamrick, Joseph T. & Withee, Joseph R., Jr. Evaluation of Centrifugal Compressor Performance With Water Injection, report, July 18, 1951; (https://digital.library.unt.edu/ark:/67531/metadc58894/: accessed May 3, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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