Behaviour of skin fatigue cracks at the corners of windows in a Comet I fuselage

dc.contributor.author	R. J. Atkinson	en_US
dc.contributor.author	W. J. Winkworth	en_US
dc.contributor.author	G. M. Norris	en_US
dc.date.accessioned	2014-10-21T15:55:33Z
dc.date.available	2014-10-21T15:55:33Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/R&M-3248	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3823
dc.description.abstract	Fatigue tests on a Comet I pressure cabin subjected to operational pressure cycles are described. Cracks at window corners are the main subject of investigation. Results are compared with earlier experiments on other Comet I pressure cabins. Conclusions are reached that appear to have some general significance.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Behaviour of skin fatigue cracks at the corners of windows in a Comet I fuselage	en_US