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Saturday, August 1, 2020 | History

3 edition of Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing found in the catalog.

Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing

Patterson, James C.

Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing

by Patterson, James C.

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  • 4 Currently reading

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

    Subjects:
  • Airplanes -- Turbine-propeller engines.

  • Edition Notes

    StatementJames C. Patterson, Jr., and Glynn R. Bartlett.
    SeriesNASA technical paper -- 2739.
    ContributionsBartlett, Glynn R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14663533M


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Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing by Patterson, James C. Download PDF EPUB FB2

Get this from a library. Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing. [James C Patterson; Glynn R Bartlett; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.]. Patterson, James C.: Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing / (Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information.

Configuration Redesign and Prototype Flight Testing of an Unmanned Fixed-Wing eVTOL Aircraft with Under-Fuselage Hover Lift and Pusher Wingtip Propulsion System.

Further evaluation of pusher. James CP Jr, Glynn RB () Evaluation of installed performance a wing-tip-mounted pusher turboprop on a semispan wing, NASA Tech PaperAugust Google Scholar 4. Lancaster OM () Jet propulsion : Ahmed F. El-Sayed. Propeller-driven aircraft.

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A greater. Wing loading affects stall speed, climb rate, takeoff and landing distance, and loading wing The performance. turn determines the design lift coefficient, and impacts drag through its effect upon wetted area and wing span.

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