IN the present paper an attempt has been made to determine the optimum aspect ratio, wing loading and fuel load ratio under certain specified design conditions. Aeroplanes with turbojet as well as with airscrew propulsion have been considered.


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    Titel :

    The Optimum Design of Long-Range Aircraft


    Untertitel :

    An Examination of the Best Values of Aspect Ratio Wing Loading and Fuel Load Ratio for Different Conditions


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1957-04-01


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Optimum design of long-range aircraft

    Sanders, K.L. | Engineering Index Backfile | 1957



    Design approach for long range aircraft

    Boname, R.V. | Engineering Index Backfile | 1943



    Fixed-range optimum trajectories for short-haul aircraft

    Erzberger, Heinz / MacLean, John D. / Barman, John F. | TIBKAT | 1975