Multiple over-all performance and rotating-stall characteristics of a 15-stage experimental axial-flow compressor at an intermediate speed

One of 5,158 reports in the series: NACA Research Memorandums available on this site.
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From Summary: "The 15-stage experimental axial-flow compressor was investigated at 78.5 percent of design speed, which falls in the region of the surge-limit line discontinuity. In this region indications of multiple characteristic curves of compressor operation had been found. On the basis of previous stage-matching analyses, these multiple performance characteristics appear to be the result of multiple-valued stage performance characteristics."

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10 p.

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Lucas, James G. & Filippi, Richard E. July 2, 1954.

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

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  • Main Title: Multiple over-all performance and rotating-stall characteristics of a 15-stage experimental axial-flow compressor at an intermediate speed
  • Series Title: NACA Research Memorandums

Description

From Summary: "The 15-stage experimental axial-flow compressor was investigated at 78.5 percent of design speed, which falls in the region of the surge-limit line discontinuity. In this region indications of multiple characteristic curves of compressor operation had been found. On the basis of previous stage-matching analyses, these multiple performance characteristics appear to be the result of multiple-valued stage performance characteristics."

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10 p.

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  • Accession or Local Control No: 93R17664
  • URL: http://hdl.handle.net/2060/19930088374 External Link
  • Report No.: NACA-RM-E54C29
  • Center for AeroSpace Information Number: 19930088374
  • Archival Resource Key: ark:/67531/metadc60749

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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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  • July 2, 1954

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • March 28, 2018, 10:31 a.m.

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Lucas, James G. & Filippi, Richard E. Multiple over-all performance and rotating-stall characteristics of a 15-stage experimental axial-flow compressor at an intermediate speed, report, July 2, 1954; (https://digital.library.unt.edu/ark:/67531/metadc60749/: accessed November 16, 2025), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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