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)
Ideas, integrated design and analysis system
SAE Paper
SAE Meeting ; 1968 Design
1968
17 pages
Aufsatz (Konferenz)
Englisch
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