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The Bending Stresses in Cantilever Plates by Moiré Fringes: An Experimental Technique giving Directly the Gradient at all Points on a Model's Surface

P.J. Palmer Ph.D., M.Sc., D.I.C., A.R.C.S., A.F.R.Ae.S., A.Inst.P. (Formerly a Lecturer at the University of Birmingham, now with John Thompson Ltd.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 December 1957

41

Abstract

The bending stresses in plate models can be determined by means of the experimentally produced moire fringes, which Rive directly the gradients at all points of the surface of the model. It is shown that this technique can be used for cantilever plates with either uniform or non‐uniform thickness provided that, in the latter case, the thickness is not large. The technique and apparatus is described, details of the experimental technique are given and discussed, and some resultant experimental fringe patterns are shown and analysed.

Citation

Palmer, P.J. (1957), "The Bending Stresses in Cantilever Plates by Moiré Fringes: An Experimental Technique giving Directly the Gradient at all Points on a Model's Surface", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 12, pp. 377-380. https://doi.org/10.1108/eb032902

Publisher

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MCB UP Ltd

Copyright © 1957, MCB UP Limited

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