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NASA NTRS ยท 19930021680

A Rayleigh-Ritz analysis methodology for cutouts in composite structures

Abstract

A new Rayleigh-Ritz stress analysis methodology that was developed for composite panels containing cutouts is described. The procedure, which makes use of a general assumed displacement field, accommodates circular and elliptical cutouts in biaxially loaded rectangular composite panels. Symmetric integral padups around the cutout can be included in the analysis. Benchmark results are presented to demonstrate the accuracy of the technique. Strength predictions based on the average stress criterion are generated and compared with experimental data. Finally, the stress analysis methodology is integrated into a design procedure for sizing integral padups around circular cutouts, and a sample problem is solved to illustrate its use.

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BibTeXRIS

Russell, Steven G.. 1991-01-01. A Rayleigh-Ritz analysis methodology for cutouts in composite structures. https://ntrs.nasa.gov/citations/19930021680

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