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Filtering by: Subject Airplanes -- Materials Remove constraint Subject: Airplanes -- Materials Degree Field Mechanical Engineering Remove constraint Degree Field: Mechanical Engineering Subject Airplanes -- Fuselage -- Testing Remove constraint Subject: Airplanes -- Fuselage -- Testing

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  • A nonlocal damage theory for laminated plate with application to aircraft damage tolerance

    Creator:
    Nahan, Matthew F.
    Abstract:
    Design of commercial aircraft structure, composed of composite material, requires the prediction of failure loads given large scale damage. In particular, a fuselage of graphite/epoxy lamination was analyzed for damage tolerance given a standard large crack that severed both skin and internal structure. Upon loading, a zone of damage is...
    Resource Type:
    Dissertation
    Full Text:
    : Timothy C. Kennedy Design of commercial aircraft structure, composed of composite material, requires the