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Component Performance Investigation of J71 Type II Turbines 3 - Overall Performance of J71 Type IIA Turbine

One of 5,157 reports in the series: NACA Research Memorandums available on this site.

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Description

"The over-all component performance characteristics of the J71 Type IIA three-stage turbine were experimentally determined over a range of speed and over-all turbine total-pressure ratio at inlet-air conditions af 35 inches of mercury absolute and 700 deg. R. The results are compared with those obtained for the J71 Type IIF turbine, which was previously investigated, the two turbines being designed for the same engine application. Geometrically the two turbines were much alike, having the same variation of annular flow area and the same number of blades for corresponding stator and rotor rows" (p. 1).

Physical Description

18 p. : ill.

Creation Information

Schum, Harold J.; Davison, Elmer H. & Petrash, Donald A. January 20, 1955.

Context

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 62 times. More information about this report can be viewed below.

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  • Main Title: Component Performance Investigation of J71 Type II Turbines 3 - Overall Performance of J71 Type IIA Turbine
  • Series Title: NACA Research Memorandums

Description

"The over-all component performance characteristics of the J71 Type IIA three-stage turbine were experimentally determined over a range of speed and over-all turbine total-pressure ratio at inlet-air conditions af 35 inches of mercury absolute and 700 deg. R. The results are compared with those obtained for the J71 Type IIF turbine, which was previously investigated, the two turbines being designed for the same engine application. Geometrically the two turbines were much alike, having the same variation of annular flow area and the same number of blades for corresponding stator and rotor rows" (p. 1).

Physical Description

18 p. : ill.

Notes

"III."

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  • URL: http://hdl.handle.net/2060/20090021651 External Link
  • Report No.: NACA-RM-E55A20
  • Center for AeroSpace Information Number: 20090021651
  • Archival Resource Key: ark:/67531/metadc65206

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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

  • January 20, 1955

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • Jan. 7, 2019, 12:41 p.m.

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Schum, Harold J.; Davison, Elmer H. & Petrash, Donald A. Component Performance Investigation of J71 Type II Turbines 3 - Overall Performance of J71 Type IIA Turbine, report, January 20, 1955; (https://digital.library.unt.edu/ark:/67531/metadc65206/: accessed April 18, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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