Some Developments and Applications of Brittle Lacquers: A Survey of Published Work and Some Original Contributions
J.R. Linge D.C.Ae., A.F.R.Ae.S.
(Group Leader, Research and Development Laboratories, Atomic Power Constructions Ltd.; formerly Test Engineer, Experimental Stress Analysis, The Fairey Aviation Co. Ltd.)
30
Abstract
A PHOTOGRAPH of the fully developed crack pattern adjacent to the end bolts in a Perspex model of the rear spar root joint of the same blade is given in FIG. 35. Fatigue tests are to be undertaken on the metal prototypes of the front and rear spar joints in which modifications arrived at by the model tests will be incorporated.
Citation
Linge, J.R. (1958), "Some Developments and Applications of Brittle Lacquers: A Survey of Published Work and Some Original Contributions", Aircraft Engineering and Aerospace Technology, Vol. 30 No. 6, pp. 173-179. https://doi.org/10.1108/eb032979
Publisher
:MCB UP Ltd
Copyright © 1958, MCB UP Limited