Analytical method presents optimum structural material/design concept that provides best balance between weight and cost for given vehicle; criterion for selection of optimum cost-weight design is dependent upon value of weight saving applied to vehicle under study; this value is derived in sample analysis of total systems costs associated with fighter aircraft; it is shown that optimum design for structures cost effectiveness may differ from minimum-weight concept, and that merit function used may be applied to any structural design problem wherein weight and cost are prominent evaluation factors; examples of applications to other design areas.


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    Titel :

    Structures cost effectiveness


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Emero, D.H. (Autor:in) / Alvey, V.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Structures cost effectiveness

    ALVEY, V. | AIAA | 1966


    Structures cost effectiveness.

    ALVEY, V. W. | AIAA | 1967


    Cost Effectiveness of Lunar Concrete for Lunar Structures

    Omar, H. A. / Issa, M. | British Library Conference Proceedings | 1993


    Cost-Effectiveness Analysis of Aesthetic Design of Expressway Structures

    Mori, Y. | British Library Conference Proceedings | 1995


    Cost-Effectiveness

    Ellis, Charles J. / Bell, Chauncey F. / Newman, Col. John T. et al. | SAE Technical Papers | 1964