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Volume 30, Issue 6
1 June 1958
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 30, Issue 6
Review Article| June 01 1958

Some Developments and Applications of Brittle Lacquers: A Survey of Published Work and Some Original Contributions

Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1958
Aircraft Engineering (1958) 30 (6): 173–179.
https://doi.org/10.1108/eb032979

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.

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© MCB UP Limited
1958
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