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THE shear stress in thinwalled tubes is often a design criterion and considerable weight economy can be effected by an exact stress determination. The problem has been investigated by D. Williams, and the principle is here elaborated and extended to form a practical and very general method which enables many types of structure to be dealt with, such as slats, ailerons, monocoque and semimonocoque wings, fuselages and tailunits in which the following diversities are encompassed
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Nov 1, 1939
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