Publication Date:
2019-08-28
Description:
Results obtained on the postbuckling behavior of plates and curved panels using the NOLIN computer program are reported. As an example, the postbuckling behavior of a flexible, isotropic and quadrangular plate is solved and the results are found to be accurate and relibale in comparison with those in the literature. The fatigue-deformation behavior of a rectangular CKL plate is measured, and the results are compared with those from NOLIN and other computer programs. A slightly curved panel with optimized layering is studied.
Keywords:
STRUCTURAL MECHANICS
Type:
NASA-TT-20094
,
NAS 1.77:20094
Format:
text