THE shear stress distribution in hollow sections subjected to bending and torsion is a subject about which there does not appear to be much information in standard text books, and a knowledge of the theory and its numerical application is becoming important to the aircraft designer in view of the increasing popularity of the stressed‐skin type of construction.
Goodey, W.J. (1936), "Shear Stresses in Hollow Sections: An Account of the Theory of Stresses in Bending and Torsion for Designers of Stressed‐Skin Structures", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 4, pp. 93-102. https://doi.org/10.1108/eb030031Download as .RIS
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