Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics

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

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Description

Report presenting the effect of compressibility on the loss characteristics downstream of two-dimensional turbomachine blade rows. In this particular example, increasing the trailing-edge thickness increased the overall loss coefficients significantly, with an effect of compressibility only at exit flow angles close to axial.

Physical Description

48 p. : ill.

Creation Information

Stewart, Warner L. July 1955.

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

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  • Main Title: Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics
  • Series Title: NACA Technical Notes

Description

Report presenting the effect of compressibility on the loss characteristics downstream of two-dimensional turbomachine blade rows. In this particular example, increasing the trailing-edge thickness increased the overall loss coefficients significantly, with an effect of compressibility only at exit flow angles close to axial.

Physical Description

48 p. : ill.

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  • Accession or Local Control No: 93R13512
  • URL: http://hdl.handle.net/2060/19930084222 External Link
  • Report No.: NACA-TN-3515
  • Center for AeroSpace Information Number: 19930084222
  • Archival Resource Key: ark:/67531/metadc57645

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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

  • July 1955

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

Description Last Updated

  • June 20, 2018, 11:37 a.m.

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Stewart, Warner L. Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics, report, July 1955; (digital.library.unt.edu/ark:/67531/metadc57645/: accessed September 25, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.