A Boeing 707 fuselage section was drop tested to measure structural, seat, and anthropomorphic dummy response to vertical crash loads. The specimen had nominally zero pitch, roll and yaw at impact with a sink speed of 20 ft/sec. Results from this drop test and other drop tests of different transport sections will be used to prepare for a full-scale crash test of a B-720.
Vertical Drop Test of a Transport Fuselage Center Section Including the Wheel Wells
1983
59 pages
Report
No indication
English
Vertical Drop Test of a Transport Fuselage Section
British Library Conference Proceedings | 2002
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SAE Technical Papers | 2002
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