This discussion summarizes the highlights of the C-141A airplane program, emphasizing fatigue, damage tolerance, and static strength considerations philosophically and in considerable detail where design criteria are involved. Dynamic considerations are also included insofar as the structural design of the airplane was affected thereby. Finally, some significant differences in criteria requirements between the C-141A and the C-5A are identified together with their expected impact on structural design.


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    Title :

    Large Cargo Airplane Structural Considerations


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966



    Publication date :

    1966-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Large cargo airplane structural considerations

    Shuler, W.T. | Engineering Index Backfile | 1966


    Design considerations of cargo airplane

    Wood, C. | Engineering Index Backfile | 1943


    Design considerations of cargo airplane

    Wood, C. | Engineering Index Backfile | 1944


    DESIGN CONSIDERATIONS of the CARGO AIRPLANE

    WOOD, CARLOS | SAE Technical Papers | 1944


    STRUCTURAL MATERIALS FOR THE CARGO AIRPLANE

    Hoekstra, H. D. | SAE Technical Papers | 1942