Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory

One of 1,424 reports in the series: NACA Technical Reports available on this site.

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Description

"The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested. The performance of the compressor was determined for speeds from 5000 to 14,000 r.p.m with varying air flow at each speed" (p. 81).

Physical Description

81 - 99 p. : ill.

Creation Information

Sinnette, John T., Jr.; Schey, Oscar W. & King, J. Austin August 1, 1944.

Context

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

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  • Main Title: Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
  • Series Title: NACA Technical Reports

Description

"The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested. The performance of the compressor was determined for speeds from 5000 to 14,000 r.p.m with varying air flow at each speed" (p. 81).

Physical Description

81 - 99 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R21127
  • URL: http://hdl.handle.net/2060/19930091837 External Link
  • Report No.: NACA-TR-758
  • Center for AeroSpace Information Number: 19930091837
  • Archival Resource Key: ark:/67531/metadc60023

Collections

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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).

Technical Report Archive and Image Library

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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Creation Date

  • August 1, 1944

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • July 5, 2018, 5:18 p.m.

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Sinnette, John T., Jr.; Schey, Oscar W. & King, J. Austin. Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory, report, August 1, 1944; (digital.library.unt.edu/ark:/67531/metadc60023/: accessed August 15, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.