Abstract: Applying the theory of non-linear finite element and transient dynamic analysis, the taper bumper device of certain aircraft ejecting device is simulated by MSC Dytran. The interrelated measures are provided within the transient impact. The analysis verifies the feasibility of the bumper and provides the basic for further test and optimization in the future.
Publication Year: 2006
Publication Date: 2006-01-01
Language: en
Type: article
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