Scatter in Fatigue:- Elements and Sections from Aircraft Structures

dc.contributor.author	A. M. Stagg	en_US
dc.date.accessioned	2014-10-20T11:06:49Z
dc.date.available	2014-10-20T11:06:49Z
dc.date.issued	1976	en_US
dc.identifier.other	ARC/CP-1357	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1370
dc.description.abstract	The fatigue test results, for elements and sections from the structures of aircraft, obtained by a number of experimenters are analysed in terms of the scatter present in the lives to fatigue failure. Data for structures made of any light alloy material and tested under any form of loading have been included in an attempt to increase the definition of any trends noted in the scatter, which was calculated using a log-normal distribution of fatigue lives as a basis. * Replaces RAE Technical Report 69155 - ARC 31639	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Scatter in Fatigue:- Elements and Sections from Aircraft Structures	en_US