The strength and stiffness design process is described in terms of its constituents. An integrated structural analysis and design system developed at Boeing, ATLAS, is described in terms of its system architecture and its technical capabilities and examples of its use are given. Finally, the basic motivation for the development of such analysis tools and the impact of design automation are considered.


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    Title :

    Aircraft strength and stiffness design automation


    Additional title:

    Automation bei der Bestimmung der Flugzeugstaerke und Steifigkeit


    Contributors:
    Thomas, R.M. (author) / Backman, B.F. (author) / Flood, F.D. (author)


    Publication date :

    1975


    Size :

    11 Seiten, 15 Bilder, 2 Tabellen, 3 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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