Computational method estimates weight of aircraft wings from theoretical relationships and empirical data. Permits comparison of alternative materials, methods of construction, and design philosophies. Method used to make tradeoffs in preliminary design phases on basis of simple input data and for more accurate calculations in later phases when more data are available.


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    Title :

    Semiempirical Estimate of Aircraft Wing Weight


    Contributors:
    York, P. (author) / Labell, R. W. (author)

    Published in:

    Publication date :

    1983-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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