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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    Title :

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


    Contributors:

    Publication date :

    1983-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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