A Boeing 707 fuselage section was drop tested at the NASA Langley Research Center to measure structural, seat, and occupant response to vertical crack loads. Post-test inspection showed that the section bottom collapsed inward approximately 2 ft. Preliminary data traces indicated maximum normal accelerations of 20 g on the fuselage bottom, 10 to 12 g on the cabin floor, and 6.5 to 8 g in the pelvises of the anthropomorphic dummies.


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    Titel :

    Vertical drop test of a transport fuselage section located forward of the wing


    Beteiligte:
    Williams, M. S. (Autor:in) / Hayduk, R. J. (Autor:in)

    Erscheinungsdatum :

    01.08.1983


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





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