Design development program for C-141 A airframe by Lockheed-Georgia Co is summarized with emphasis on fatigue, damage tolerance, and static strength considerations; fatigue design criteria used for C-141A and C-5A are considered in detail; some significant differences in criteria requirements between C-141A and C-5A are identified together with expected impact on structural design.


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    Titel :

    Large cargo airplane structural considerations


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Shuler, W.T. (Autor:in)

    Kongress:

    SAE Meeting ; 1966 Design



    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Large Cargo Airplane Structural Considerations

    Shuler, W. T. | SAE Technical Papers | 1966


    Design considerations of cargo airplane

    Wood, C. | Engineering Index Backfile | 1944


    Design considerations of cargo airplane

    Wood, C. | Engineering Index Backfile | 1943


    Design considerations of cargo airplane

    Wood, C. | Engineering Index Backfile | 1943


    DESIGN CONSIDERATIONS of the CARGO AIRPLANE

    WOOD, CARLOS | SAE Technical Papers | 1944