Loads Development for two Aircraft Fuselages using FAR criteria and parametrised FE-models

PC Astori, J. Hupperets, MJL van Tooren

    Research output: Book/ReportReportScientific


    This report describes a preliminary structural analysis of 2 complete fuselages, both belonging to the jet airliner category and differing for passenger capacity: 100 and 350 passengers respectively; the analysis is done for a set of loading conditions considered relevant for the aircraft category, and is aimed to provide data for material selection for different areas of the fuselage.
    Original languageUndefined/Unknown
    Place of PublicationDelft
    PublisherDelft University of Technology
    Number of pages114
    Publication statusPublished - 2003

    Publication series

    PublisherTU Delft

    Bibliographical note

    CD-rom, hardcopy


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