Application of radial-equilibrium condition to axial-flow turbomachine design including consideration of change of entropy with radius downstream of blade row

One of 5,164 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting an investigation of the validity of application of the simplified-radial-equilibrium equation to axial-flow turbomachines. Two different types of equations were used. Results regarding the interpretation of the data, single stages, middle and end stages of the multistage compressor, application of the radial-equilibrium equation, and the solution for the velocity distributions are provided.

Physical Description

52 p. : ill.

Creation Information

Hatch, James E.; Giamati, Charles C. & Jackson, Robert J. April 14, 1954.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 411 times , with 10 in the last month . More information about this report can be viewed below.

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  • Main Title: Application of radial-equilibrium condition to axial-flow turbomachine design including consideration of change of entropy with radius downstream of blade row
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation of the validity of application of the simplified-radial-equilibrium equation to axial-flow turbomachines. Two different types of equations were used. Results regarding the interpretation of the data, single stages, middle and end stages of the multistage compressor, application of the radial-equilibrium equation, and the solution for the velocity distributions are provided.

Physical Description

52 p. : ill.

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  • Accession or Local Control No: 93R17438
  • URL: http://hdl.handle.net/2060/19930088148 External Link
  • Report No.: NACA-RM-E54A20
  • Center for AeroSpace Information Number: 19930088148
  • Archival Resource Key: ark:/67531/metadc60256

Collections

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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

  • April 14, 1954

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • May 31, 2018, 5:29 p.m.

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Hatch, James E.; Giamati, Charles C. & Jackson, Robert J. Application of radial-equilibrium condition to axial-flow turbomachine design including consideration of change of entropy with radius downstream of blade row, report, April 14, 1954; (digital.library.unt.edu/ark:/67531/metadc60256/: accessed September 25, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.