SEDL / STP / STP972-EB / STP26135S



An Experimental Study of a Curved Composite Panel with a Cutout

Palazotto, AN
Professor, Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio


Pages: 12    Published: Jan 1988


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Abstract

This paper is an attempt to compare a set of experimental measurements on a panel with a symmetrically positioned cutout to values determined through a nonlinear finite element program. The comparison shows the sensitivity of the panel to a varying boundary condition produced by the restraints associated with the experimental structure. The finite element program used is STAGS C-1.


Keywords:
composite material, collapse load, experimentation, panels, cutouts

Paper ID: STP26135S
Committee/Subcommittee: D30.02
DOI: 10.1520/STP26135S
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