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发表于 2013-3-31 07:39:25
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来自 北京
LINK1 Assumptions and Restrictions
The spar element assumes a straight bar, axially loaded at its ends, of uniform properties from end to end.
The length of the spar must be greater than zero, so nodes I and J must not be coincident.
The spar must lie in an X-Y plane and must have an area greater than zero.
The temperature is assumed to vary linearly along the length of the spar.
The displacement shape function implies a uniform stress in the spar.
The initial strain is also used in calculating the stress stiffness matrix, if any, for the first cumulative iteration.
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