Method uses formulas based on theoretical ideal wing; predicted weight attained by multiplying weight of ideal wing by correction factor derived from statistical analysis of actual wing weights; method provides designer with yardstick by which to compare alternative designs and indicates where improvement might be effected.


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    Title :

    Estimation of wing weight


    Additional title:

    Aircraft Eng


    Contributors:
    Solvey, J. (author)

    Published in:

    Publication date :

    1951


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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