Propulsion system requirements of very long range, high payload aircraft relative to propulsion and laminar flow control are examined with emphasis on turbofan engines; factors influencing optimum design bypass ratio of turbofan engine and effects of laminar flow control and cargo space requirements upon optimum turbofan engine design are shown; parametric study of aircraft performance is used to compare series of industry study engines as means of showing relationship between aircraft and engine design; mission studies included offensive and defensive armed logistics, command and surveillance.


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    Titel :

    Requirements for long range -- Long endurance aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Wheaton, R.J. (Autor:in) / Bogdanovic, J.A. (Autor:in) / Feder, A. (Autor:in)

    Kongress:

    SAE Meeting ; 1964



    Erscheinungsdatum :

    1964


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT

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


    Method of determining propulsion system requirements for long-range, long-endurance aircraft

    Bogdanovic, J.A. / Feder, A. / Wheaton, R.J. | Engineering Index Backfile | 1965




    Aircraft for Long Range and Long Endurance Missions

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