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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    Title :

    The Optimum Design of Long-Range Aircraft


    Subtitle :

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


    Contributors:

    Published in:

    Publication date :

    1957-04-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Optimum design of long-range aircraft

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



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



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