Compression buckling analysis of flat panels with Z-section stiffeners

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Abstract

NACA conducted extensive tests of z-stiffened panels under compressive load in the 1940s and 1950s in order to create direct-reading design charts. Because of the asymmetry of z-stiffened panels, the buckling behavior is complex and buckling analysis of the NACA data has not been conducted. In order to analyze the buckling of z-stiffened panels, a new tool for the buckling analysis of thin-walled structures is developed. This paper presents the results of the buckling analysis of the NACA data and investigates the buckling behavior of z-stiffened panels. It is found that the lateral buckling of the stiffener is critical in the short column region, while the torsional buckling of the stiffener is not critical.

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APA

Taki, T. (2017). Compression buckling analysis of flat panels with Z-section stiffeners. In Transactions of the Japan Society for Aeronautical and Space Sciences (Vol. 60, pp. 171–180). Japan Society for Aeronautical and Space Sciences. https://doi.org/10.2322/tjsass.60.171

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