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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    Title :

    Requirements for long range -- Long endurance aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1964



    Publication date :

    1964


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT

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


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    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