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.
Vertical drop test of a transport fuselage section located forward of the wing
1983-08-01
Report
No indication
English
Vertical Drop Test of a Transport Fuselage Section
British Library Conference Proceedings | 2002
|Vertical Drop Test of a Transport Fuselage Section
SAE Technical Papers | 2002
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