Calculated performance and weight data are presented for proposed VTOL aircraft powerplant, which uses highly loaded fans immersed in wings to augment thrust of conventional turbojet engines for hovering; thrust augmentation ratio, shown to be of order of 3.5, implies satisfactory matching of cruising and hovering capabilities of powerplant for high-altitude flight, but surplus of cruising thrust is produced for short low-altitude missions.


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    Titel :

    Fan-in-wing powerplant system for VTOL aircraft


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:
    Cockshutt, E.P. (Autor:in) / Galitzine, N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lift-thrust powerplant arrangement for commercial VTOL aircraft

    Tyler, R.A. | Engineering Index Backfile | 1962



    Jet powerplant requirements for VTOL

    Hewson, C.T. | Engineering Index Backfile | 1959


    Powerplant aspects of high-speed, inter-city VTOL aircraft

    Pickerell, D.J. / Cresswell, R.A. | Engineering Index Backfile | 1968


    VTOL AIRCRAFT WING

    KIRIAKIDI SERGEJ KONSTANTINOVICH / POPOV DMITRIJ PAVLOVICH / TUPITSYN ALEKSANDR PAVLOVICH | Europäisches Patentamt | 2015

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