原文传递
Vertical drop test of a transport fuselage section located forward of the wing
| 题名： | Vertical drop test of a transport fuselage section located forward of the wing |
| 作者： | Williams, M. S.; Hayduk, R. J. |
| 关键词： | section；vertical；forward；transport；loca；fuse；ocat；drop；test；inspection |
| 摘要： | 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. |
| 报告类型： | 科技报告 |
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