System, designated IDEAS, is new approach directed toward rapid definition of design loading conditions and internal structural element loads needed for sizing and analysis of primary structure of entire aircraft; it is integrated collection of many computer programs and formalized calculations which are performed in particular sequence; system treats all applicable flight maneuvers, landing and catapult conditions, taxing conditions, gust and flutter analysis; it enables calculation of all applied air, inertia and ground loads, together with all internal structural load distributions within short time periods. (17339)


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    Title :

    Ideas, integrated design and analysis system


    Additional title:

    SAE Paper


    Contributors:

    Conference:

    SAE Meeting ; 1968 Design


    Published in:

    Publication date :

    1968


    Size :

    17 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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