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Shock and Vibration
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2017
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Article
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Tab 4
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Research Article
A Numerical-Experimental Method for Drop Impact Analysis of Composite Landing Gear
Table 4
Parameters of the drop impact analysis.
Number
Equivalent mass/kg
Height/m
AOA/°
A
120
0.136
0
B
131
0.46
0
C
136
0.46
12