The structural, manufacturing, and service and environmental considerations that could impact the design of composite fuselage structure for commercial transport aircraft application were explored. The severity of these considerations was assessed and the principal design drivers delineated. Technical issues and potential problem areas which must be resolved before sufficient confidence is established to commit to composite materials were defined. The key issues considered are: definition of composite fuselage design specifications, damage tolerance, and crashworthiness.


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    Title :

    Design Considerations for Composite Fuselage Structure of Commercial Transport Aircraft


    Contributors:
    G. W. Davis (author) / I. F. Sakata (author)

    Publication date :

    1981


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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