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Thursday, May 14, 2020 | History

3 edition of Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine found in the catalog.

Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine

Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine

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Published by National Aeronautics and Space Administration in [Washington, D.C.? .
Written in English

    Subjects:
  • Boundary layer.,
  • Turbines -- Aerodynamics.

  • Edition Notes

    StatementKestutis C. Civinskas and Louis A. Povinelli.
    SeriesNASA technical memorandum -- 83669., USAAVSCOM technical report -- 84-C-1., AVSCOM technical report -- 84-C-1.
    ContributionsPovinelli, Louis A., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18040012M


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Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine Download PDF EPUB FB2