A COMPILATION of formulae and data from the article on the same subject in the July 1971 issue of AIRCRAFT ENGINEERING is presented to enable weight engineers to make a quick estimation of wing structural weight for preliminary aircraft design. Application of the method to 46 samples of aircraft in a wide range of sizes demonstrates a standard deviation of 9·64 per cent, satisfactory for point designs and parametric studies.


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    Titel :

    Quick estimation of wing structural weight for preliminary aircraft design


    Beteiligte:
    TORENBEEK, E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-02-01


    Format / Umfang :

    2 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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