Application of supersonic vortex-flow theory to the design of supersonic impulse compressor- or turbine-blade sections

One of 5,163 reports in the series: NACA Research Memorandums available on this site.

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Description

From Introduction: "The purpose of this paper is to present an analytical method for the design of two-dimensional related selection of a blade for particular rotor conditions may be made quickly and easily and its performance deduced from tests of representative sections in cascade."

Physical Description

70 p. : ill.

Creation Information

Boxer, Emanuel; Sterrett, James R. & Wlodarski, John April 24, 1952.

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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 972 times , with 41 in the last month . More information about this report can be viewed below.

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  • Main Title: Application of supersonic vortex-flow theory to the design of supersonic impulse compressor- or turbine-blade sections
  • Series Title: NACA Research Memorandums

Description

From Introduction: "The purpose of this paper is to present an analytical method for the design of two-dimensional related selection of a blade for particular rotor conditions may be made quickly and easily and its performance deduced from tests of representative sections in cascade."

Physical Description

70 p. : ill.

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  • Accession or Local Control No: 93R16302
  • URL: http://hdl.handle.net/2060/19930087012 External Link
  • Report No.: NACA-RM-L52B06
  • Center for AeroSpace Information Number: 19930087012
  • Archival Resource Key: ark:/67531/metadc59156

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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 24, 1952

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 9, 2018, 11:49 a.m.

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Boxer, Emanuel; Sterrett, James R. & Wlodarski, John. Application of supersonic vortex-flow theory to the design of supersonic impulse compressor- or turbine-blade sections, report, April 24, 1952; (digital.library.unt.edu/ark:/67531/metadc59156/: accessed May 28, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.