Application of a characteristic blade-to-blade solution to flow in a supersonic rotor with varying stream-filament thickness

One of 4,119 reports in the series: NACA Technical Notes available on this site.

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Description

From Introduction: "A solution of the type of reference 2 is necessary to give the stream-sheet thickness and curvature for the blade-to-blade (S1 surface) solution considered in this report. The equations for the solution of the S1 surface of revolution are presented in reference 3. The purpose of the subject report is to continue the work of reference 3 by applying the method to a specific problem in order that the practicability of the method and the time involved in computing a solution may be determined."

Physical Description

36 p. : ill.

Creation Information

Costilow, Eleanor L. August 1953.

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

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  • Main Title: Application of a characteristic blade-to-blade solution to flow in a supersonic rotor with varying stream-filament thickness
  • Series Title: NACA Technical Notes

Description

From Introduction: "A solution of the type of reference 2 is necessary to give the stream-sheet thickness and curvature for the blade-to-blade (S1 surface) solution considered in this report. The equations for the solution of the S1 surface of revolution are presented in reference 3. The purpose of the subject report is to continue the work of reference 3 by applying the method to a specific problem in order that the practicability of the method and the time involved in computing a solution may be determined."

Physical Description

36 p. : ill.

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  • Accession or Local Control No: 93R13022
  • URL: http://hdl.handle.net/2060/19930083732 External Link
  • Report No.: NACA-TN-2992
  • Center for AeroSpace Information Number: 19930083732
  • Archival Resource Key: ark:/67531/metadc56806

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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

  • August 1953

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

Description Last Updated

  • April 9, 2018, 11:46 a.m.

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Costilow, Eleanor L. Application of a characteristic blade-to-blade solution to flow in a supersonic rotor with varying stream-filament thickness, report, August 1953; (digital.library.unt.edu/ark:/67531/metadc56806/: accessed December 10, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.