Experimental Investigation of Ultimate Loads Carried by Flat, Unstiffened Panels Under Combined Shear and Compression

<p>Four series of tests were made on flat, unstiffened panels under combined shear and compression loading for two thicknesses and two length over width ratios. In each case, the panels were carried to their ultimate loads. An empirical relation was developed for the variation of shear and c...

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Bibliographic Details
Main Author: Butterworth, Wesley Theodore
Format: Others
Published: 1938
Online Access:https://thesis.library.caltech.edu/5150/1/Butterworth_wt_1938.pdf
Butterworth, Wesley Theodore (1938) Experimental Investigation of Ultimate Loads Carried by Flat, Unstiffened Panels Under Combined Shear and Compression. Master's thesis, California Institute of Technology. doi:10.7907/C57T-2C92. https://resolver.caltech.edu/CaltechETD:etd-12282005-095455 <https://resolver.caltech.edu/CaltechETD:etd-12282005-095455>
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Summary:<p>Four series of tests were made on flat, unstiffened panels under combined shear and compression loading for two thicknesses and two length over width ratios. In each case, the panels were carried to their ultimate loads. An empirical relation was developed for the variation of shear and compressive stresses of the form: (P<sub>c</sub>/P<sub>c<sub>o</sub></sub>) + (P<sub>s</sub>/P<sub>s<sub>o</sub></sub>)<sup>4</sup> = 1, <br /> where:<br /> P<sub>c<sub>o</sub></sub> = failure stress, pure compression,<br /> P<sub>s<sub>o</sub></sub> = failure stress, pure shear. <br /> The above equation was found to hold for the entire range of thicknesses and length over width ratios investigated.</p>