Results from a continuing effort to develop automated methods for structural design are described. A system of computer programs presently under development called SAVES is intended to automate the preliminary structural design of a complete aerospace vehicle. Each step in the automated design process of the SAVES system of programs is discussed, with emphasis placed on use of automated routines for generation of finite-element models. The versatility of these routines is demonstrated by structural models generated for a space shuttle orbiter, an advanced technology transport,n hydrogen fueled Mach 3 transport. Illustrative numerical results are presented for the Mach 3 transport wing.


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    Titel :

    Automated procedures for sizing aerospace vehicle structures /SAVES/


    Beteiligte:
    Giles, G. L. (Autor:in) / Blackburn, C. L. (Autor:in) / Dixon, S. C. (Autor:in)

    Kongress:

    Structures, Structural Dynamics, and Materials Conference ; 1972 ; San Antonio, TX


    Erscheinungsdatum :

    01.04.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Automated Procedures for Sizing Aerospace Vehicle Structures (SAVES)

    GARY L. GILES / CHARLES L. BLACKBURN AND SIDNEY C. DIXON | AIAA | 1972


    Automated procedures for sizing aerospace vehicle structures /SAVES/

    GILES, G. / BLACKBURN, C. / DIXON, S. | AIAA | 1972