THE uses of high‐tensile aluminium alloy compression members in aircraft construction may be divided into two main classes: (1) That in which the members are employed as stiffeners in stresscd‐skin construction; (2) That in which they are employed as struts in trussed structures.
Dudley, L.P. (1941), "Buckling Strength of Duralumin Columns: A Simple Graphical Method of Predicting the Behaviour of a Long Columnar Strut in this Alloy", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 10, pp. 281-283. https://doi.org/10.1108/eb030831
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