Performance of Compressor of Xj-41-v Turbojet Engine v-Performance Analysis of Compressor With Revised Vaned Collector Over Range of Compressor Speeds From 3600 to 11,500 RPM

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

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Description

"An investigation of the XJ-41-V turbojet-engine compressor with a revised vaned collector was conducted to determine the performance of the compressor and to obtain fundamental information on the aerodynamic problems associated with large centrifugal compressors of this type. The original vaned collector was revised by increasing the flow area at the vaned collector entrance. A maximum adiabatic efficiency of 0.81 was obtained at a corrected weight flow of 36.5 pounds per second and a pressure ratio of 1.90" (p. 1).

Physical Description

21 p. : ill.

Creation Information

Ginsburg, Ambrose; Creagh, John W. R. & Michel, Donald January 23, 1948.

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

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  • Main Title: Performance of Compressor of Xj-41-v Turbojet Engine v-Performance Analysis of Compressor With Revised Vaned Collector Over Range of Compressor Speeds From 3600 to 11,500 RPM
  • Series Title: NACA Research Memorandums

Description

"An investigation of the XJ-41-V turbojet-engine compressor with a revised vaned collector was conducted to determine the performance of the compressor and to obtain fundamental information on the aerodynamic problems associated with large centrifugal compressors of this type. The original vaned collector was revised by increasing the flow area at the vaned collector entrance. A maximum adiabatic efficiency of 0.81 was obtained at a corrected weight flow of 36.5 pounds per second and a pressure ratio of 1.90" (p. 1).

Physical Description

21 p. : ill.

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  • URL: http://hdl.handle.net/2060/20090012434 External Link
  • Report No.: NACA-RM-SE8A22
  • Center for AeroSpace Information Number: 20090012434
  • Archival Resource Key: ark:/67531/metadc65008

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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 23, 1948

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

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  • July 30, 2018, 2:46 p.m.

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Ginsburg, Ambrose; Creagh, John W. R. & Michel, Donald. Performance of Compressor of Xj-41-v Turbojet Engine v-Performance Analysis of Compressor With Revised Vaned Collector Over Range of Compressor Speeds From 3600 to 11,500 RPM, report, January 23, 1948; (digital.library.unt.edu/ark:/67531/metadc65008/: accessed October 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.