Buckling And Postbuckling Behavior Of Compression Loaded Isotropic Plates With Cutouts


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Buckling and Postbuckling Behavior of Compression-Loaded Isotropic Plates with Cutouts


Buckling and Postbuckling Behavior of Compression-Loaded Isotropic Plates with Cutouts

Author: National Aeronautics and Space Adm Nasa

language: en

Publisher: Independently Published

Release Date: 2018-10-24


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An experimental study of the buckling and postbuckling behavior of square and rectangular compression loaded aluminum plates with centrally located circular, square, and elliptical cutouts is presented. Experimental results indicate that the plates exhibit overall trends of increasing buckling strain and decreasing initial postbuckling stiffness with increasing cutout width. Corresponding plates with circular and square cutouts of the same width buckle at approximately the same strain level, and exhibit approximately the same initial postbuckling stiffness. Results show that the reduction in initial postbuckling stiffness due to a cutout generally decreases as the plate aspect ratio increases. Other results presented indicate that square plates with elliptical cutouts having a large cutout-width-to-plate-width ratio generally lose prebuckling and initial postbuckling stiffness as the cutout height increases. However, the plates buckle at essentially the same strain level. Results also indicate that postbuckling stiffness is more sensitive to changes in elliptical cutout height than are prebuckling stiffness and buckling strain. Nemeth, Michael P. Langley Research Center RTOP 505-63-01-08

Buckling and Postbuckling Behavior of Compression-loaded Isotropic Plates with Cutouts


Buckling and Postbuckling Behavior of Compression-loaded Isotropic Plates with Cutouts

Author: Michael P. Nemeth

language: en

Publisher:

Release Date: 1990


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