TY  - JOUR
AB  - 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.
VL  - 11
IS  - 1
SN  - 0002-2667
DO  - 10.1108/eb030421
UR  - https://doi.org/10.1108/eb030421
AU  - Shanley F.R.
PY  - 1939
Y1  - 1939/01/01
TI  - Engineering Aspects of Buckling: The Buckling of Simple Columns and Flat Plates Simply Explained for the Engineer
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 13
EP  - 20
Y2  - 2024/05/10
ER  -