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Extension of Useful Operating Range of Axial-Flow Compressors by Use of Adjustable Stator Blades

One of 257 reports in the series: NACA Advanced Confidential Reports available on this site.

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Description

"A theory has been developed for resetting the blade angles of an axial-flow compressor in order to improve the performance at speeds and flows other than the design and thus extend the useful operating range of the compressor. The theory is readily applicable to the resetting of both rotor and stator blades or to the resetting of only the stator blades and is based on adjustment of the blade angles to obtain lift coefficients at which the blades will operate efficiently. Calculations were made for resetting the stator blades of the NACA eight-stage axial-flow compressor for 75 percent of design … continued below

Physical Description

425 - 452 p. : ill.

Creation Information

Sinnette, John T., Jr. & Voss, William J. December 29, 1944.

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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 4147 times, with 13 in the last month. More information about this report can be viewed below.

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Description

"A theory has been developed for resetting the blade angles of an axial-flow compressor in order to improve the performance at speeds and flows other than the design and thus extend the useful operating range of the compressor. The theory is readily applicable to the resetting of both rotor and stator blades or to the resetting of only the stator blades and is based on adjustment of the blade angles to obtain lift coefficients at which the blades will operate efficiently. Calculations were made for resetting the stator blades of the NACA eight-stage axial-flow compressor for 75 percent of design speed and a series of load coefficients ranging from 0.28 to 0.70 with rotor blades left at the design setting" (p. 425).

Physical Description

425 - 452 p. : ill.

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  • Accession or Local Control No: 93R21270
  • URL: http://hdl.handle.net/2060/19930091980 External Link
  • Report No.: NACA-TR-915
  • Report No.: NACA-ACR-E6E02
  • Center for AeroSpace Information Number: 19930091980
  • Archival Resource Key: ark:/67531/metadc60225

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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

  • December 29, 1944

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • July 5, 2018, 5:16 p.m.

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Sinnette, John T., Jr. & Voss, William J. Extension of Useful Operating Range of Axial-Flow Compressors by Use of Adjustable Stator Blades, report, December 29, 1944; (https://digital.library.unt.edu/ark:/67531/metadc60225/: accessed January 18, 2025), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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