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. http://resolver.caltech.edu/CaltechETD:etd-12282005-095455
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. 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: [...] + [...] = 1, where: [...] = failure stress, pure compression, [...] = failure stress, pure shear. The above equation was found to hold for the entire range of thicknesses and length over width ratios investigated.
|Item Type:||Thesis (Master's thesis)|
|Subject Keywords:||Aeronautical Engineering|
|Degree Grantor:||California Institute of Technology|
|Division:||Engineering and Applied Science|
|Thesis Availability:||Public (worldwide access)|
|Defense Date:||1 January 1938|
|Default Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Imported from ETD-db|
|Deposited On:||29 Dec 2005|
|Last Modified:||26 Oct 2016 22:28|
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