The Behaviour of Curved Panels in Compression
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 February 1946
Abstract
THE work described in these two reports is entirely experimental and comprises a detailed investigation into the effect of size and width of panel, edge conditions, grain of material, and initial imperfections on the behaviour of curved panels under axial compression. Owing to the large number of variables, an extensive series of tests was inevitable, if useful results were to be obtained, and at the start of the work considerable trouble was taken to devise apparatus that would combine reliability of test results with rapidity of testing.
Citation
(1946), "The Behaviour of Curved Panels in Compression", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 2, pp. 56-59. https://doi.org/10.1108/eb031337
Publisher
:MCB UP Ltd
Copyright © 1946, MCB UP Limited