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Friday, July 24, 2020 | History

2 edition of Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade found in the catalog.

Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade

John F. Kline

Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade

by John F. Kline

  • 43 Want to read
  • 8 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service in [Washington], Springfield, Va .
Written in English

    Subjects:
  • Turbines -- Aerodynamics.,
  • Turbines -- Blades -- Cooling.

  • Edition Notes

    StatementJohnF. Kline, Roy G. Stabe, and Thomas P. Moffitt.
    SeriesNASA technical paper ; 1136, NASA technical paper -- 1136.
    ContributionsStabe, Roy G., Moffitt, Thomas P., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
    The Physical Object
    Pagination46 p. :
    Number of Pages46
    ID Numbers
    Open LibraryOL15225573M


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Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade by John F. Kline Download PDF EPUB FB2