Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests

One of 4,120 reports in the series: NACA Technical Notes available on this site.

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Description

From Summary: "Previous tests of blower-blade sections have been extended by a series of tests at 52.5 degrees stagger. The results of these tests have been combined with the earlier test results and are presented in new blade design charts which supersede those previously presented. An investigation in a test blower over a range of stagger from 44 degrees to 65 degrees has shown that for blades at a solidity of 1.0, the two-dimensional cascade data predict the turning angle to within 1/2 degrees."

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[21] p.

Creation Information

Bogdonoff, Seymour M. & Hess, Eugene E. April 1947.

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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 894 times , with 8 in the last month . More information about this report can be viewed below.

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  • Main Title: Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests
  • Series Title: NACA Technical Notes

Description

From Summary: "Previous tests of blower-blade sections have been extended by a series of tests at 52.5 degrees stagger. The results of these tests have been combined with the earlier test results and are presented in new blade design charts which supersede those previously presented. An investigation in a test blower over a range of stagger from 44 degrees to 65 degrees has shown that for blades at a solidity of 1.0, the two-dimensional cascade data predict the turning angle to within 1/2 degrees."

Physical Description

[21] p.

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  • Accession or Local Control No: 93R11164
  • URL: http://hdl.handle.net/2060/19930081874 External Link
  • Report No.: NACA-TN-1271
  • Center for AeroSpace Information Number: 19930081874
  • Archival Resource Key: ark:/67531/metadc55159

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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

  • April 1947

Added to The UNT Digital Library

  • Nov. 14, 2011, 10:28 p.m.

Description Last Updated

  • March 28, 2018, 9:59 a.m.

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Bogdonoff, Seymour M. & Hess, Eugene E. Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests, report, April 1947; (digital.library.unt.edu/ark:/67531/metadc55159/: accessed October 19, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.