Geometric Non-Linear Influence of a Payload Fairing on Dynamic Displacement Response
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Abstract Finite element method using three noded plate and shell element and 3D beam element in conjunction with mode superposition method is used for studying the large dynamic displacement response of a typical payload fairing due to separation impulse. Incremental technique is used for solving the geometric non-linear problem. Linear formulations are assumed and a step-by-step analysis is performed on the deformed state of each previous time step. The geometry is updated and the stiffness matrix recomputed after every finite time step and the eigenvalue analysis repeated.
2001 ◽
Vol 245
(3)
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pp. 562-570
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1990 ◽
Vol 10
(1)
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pp. 33-58
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2003 ◽
Vol 56
(15)
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pp. 2387-2408
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2009 ◽
Vol 80
(13)
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pp. 1640-1686
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1994 ◽
Vol 37
(22)
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pp. 3825-3842
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