Performance of Compressor of XJ-41-V Turbojet Engine 6 - Analysis of Compressor Flow Choking

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Description

"An extended analysis was made of the previously reported performance investigation of the original compressor from the XJ-41-V turbojet engine and a similar compressor revised a to obtain a 33-percent increase in the geometric passage area at the vaned-collector entrance. This analysis was based on the concept of the vaned-collector entrance as the throat section of a nozzle. Because of nonuniform air distribution at the vaned-collector entrance, approximately 90 percent of the available flow area was utilized in the original compressor and 94 percent in the revised compressor" (p. 1).

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12 p.

Creation Information

Creagh, John W. R. & Ginsburg, Ambrose March 23, 1948.

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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 203 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 6 - Analysis of Compressor Flow Choking
  • Series Title: NACA Research Memorandums

Description

"An extended analysis was made of the previously reported performance investigation of the original compressor from the XJ-41-V turbojet engine and a similar compressor revised a to obtain a 33-percent increase in the geometric passage area at the vaned-collector entrance. This analysis was based on the concept of the vaned-collector entrance as the throat section of a nozzle. Because of nonuniform air distribution at the vaned-collector entrance, approximately 90 percent of the available flow area was utilized in the original compressor and 94 percent in the revised compressor" (p. 1).

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12 p.

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  • URL: http://hdl.handle.net/2060/20090011946 External Link
  • Report No.: NACA-RM-SE8C12
  • Center for AeroSpace Information Number: 20090011946
  • Archival Resource Key: ark:/67531/metadc64998

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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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  • March 23, 1948

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

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  • July 30, 2018, 2:48 p.m.

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Creagh, John W. R. & Ginsburg, Ambrose. Performance of Compressor of XJ-41-V Turbojet Engine 6 - Analysis of Compressor Flow Choking, report, March 23, 1948; (https://digital.library.unt.edu/ark:/67531/metadc64998/: accessed May 16, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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