Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers

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Description

From Introduction: "Results obtained in the experimental investigations of secondary flows in turbomachines (refs. 1 to 3) indicate that information concerning three-dimensional laminar boundary-layer behavior can be of practical value in interpreting and correlating measurements of losses in the turbo-machines for design purposes. Reference 4 gives a theoretical analysis of the overturning (more than mainstream turning) of the three-dimensional laminar boundary layer developed on flat or nearly flat surfaces, under mainstream flows which consist of streamline translates (i.e., the entire streamline pattern can be obtained by translating any particular streamline pattern can be obtained by translating any particular streamline parallel … continued below

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22 p. : ill.

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Hansen, Arthur G. & Herzig, Howard Z. November 1956.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 102 times. More information about this report can be viewed below.

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  • Main Title: Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers
  • Series Title: NACA Technical Notes

Description

From Introduction: "Results obtained in the experimental investigations of secondary flows in turbomachines (refs. 1 to 3) indicate that information concerning three-dimensional laminar boundary-layer behavior can be of practical value in interpreting and correlating measurements of losses in the turbo-machines for design purposes. Reference 4 gives a theoretical analysis of the overturning (more than mainstream turning) of the three-dimensional laminar boundary layer developed on flat or nearly flat surfaces, under mainstream flows which consist of streamline translates (i.e., the entire streamline pattern can be obtained by translating any particular streamline pattern can be obtained by translating any particular streamline parallel to the leading edge, fig. 1) with constant axial velocity component."

Physical Description

22 p. : ill.

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  • Accession or Local Control No: 93R13898
  • URL: http://hdl.handle.net/2060/19930084608 External Link
  • Report No.: NACA-TN-3840
  • Center for AeroSpace Information Number: 19930084608
  • Archival Resource Key: ark:/67531/metadc56152

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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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  • November 1956

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • April 19, 2018, 10:10 a.m.

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Hansen, Arthur G. & Herzig, Howard Z. Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers, report, November 1956; (https://digital.library.unt.edu/ark:/67531/metadc56152/: accessed March 28, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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