Last edited by Taulmaran
Tuesday, November 24, 2020 | History

2 edition of Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude found in the catalog.

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude

David M Straight

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude

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  • 33 Currently reading

Published by National Aeronautics and Space Administration Scieentific and Technical Information Branch, For sale by the National Technical Information Service] in Washington D.C, [Springfield, Va .
Written in English

    Subjects:
  • Airplanes -- Turbojet engines,
  • Airplanes -- Flight testing,
  • Airplanes -- Motors -- Thrust

  • Edition Notes

    StatementDavid M. Straight and Richard R. Cullom
    SeriesNASA technical paper -- 2171
    ContributionsCullom, Richard R, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
    The Physical Object
    Pagination36 p. :
    Number of Pages36
    ID Numbers
    Open LibraryOL14933382M


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Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude by David M Straight Download PDF EPUB FB2