Paper presents parametric study to ascertain trade-off between range and endurance vs design cruise speed for aircraft powered by turbofan, cruise fan, and turboprop propulsion systems; potential for each type of propulsion system is projected for various design configurations and results of several studies indicate effects of ground rule changes, mixed power plant arrangements, and refueling; pertinence to logistics aircraft systems.


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    Titel :

    Aircraft for long range and long endurance missions


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Boyles, Jr., R.Q. (Autor:in) / Barnett, L. (Autor:in)

    Kongress:

    SAE Meeting ; 1964



    Erscheinungsdatum :

    1964


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aircraft for Long Range and Long Endurance Missions

    Barnett, Lane / Boyles, Richard Q. | SAE Technical Papers | 1964


    Requirements for long range -- Long endurance aircraft

    Wheaton, R.J. / Bogdanovic, J.A. / Feder, A. | Engineering Index Backfile | 1964


    REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT

    Feder, A. / Bogdanovic, J.A. / Wheaton, R.J. | SAE Technical Papers | 1964


    Long endurance aircraft

    PEARSON JEROME | Europäisches Patentamt | 2016

    Freier Zugriff

    Propulsion System Technologies for Long Range and Long Endurance Aircraft

    Garwood, K. R. / North Atlantic Treaty Organization | British Library Conference Proceedings | 1993