FOR the past fifteen years nearly all aircraft structures have been of the shell or stressed‐skin type and problems pertaining to this type of structure have been steadily tackled and finally solved for practical use by the designers.
Mordellet, R.L. (1950), "A Solution to the Problem of Torsion‐Flexure: A Method of Using the Principle of Least Work and Calculus of Variations to Establish the Potential Energy Integrals", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 11, pp. 335-337. https://doi.org/10.1108/eb031965
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