MOST of the structural analysis problems that have resulted from the use of “thin‐walled” construction seem to fall into two general classes: Stress distribution and buckling. Even these classes cannot be entirely separated, as the stress distribution can be greatly affected by buckling phenomena. A thorough understanding of the general principles of buckling (or structural instability) is therefore essential for efficient and safe design of modern aircraft structures.
Shanley, F.R. (1939), "Engineering Aspects of Buckling: The Buckling of Simple Columns and Flat Plates Simply Explained for the Engineer", Aircraft Engineering and Aerospace Technology, Vol. 11 No. 1, pp. 13-20. https://doi.org/10.1108/eb030421Download as .RIS
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