A Computational Method for Dynamic Analysis of Deployable Structures

Figure 9

Axial strain for the deployable structure during the motion process. (a) Time: 0.2 s. (b) Time: 0.6 s. (c) Time: 1 s. (d) Time: 1.4 s. (e) Time: 1.8 s. (f) Time: 2.2 s.

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(b)

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