The case for factors of safety of 1.5 instead of 2.0, with special reference to the flight envelope

dc.contributor.author	P. E. Montagnon	en_US
dc.date.accessioned	2014-10-21T15:50:36Z
dc.date.available	2014-10-21T15:50:36Z
dc.date.issued	1944	en_US
dc.identifier.other	ARC/R&M-2578	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2944
dc.description.abstract	The purpose of this note is to show the desirability of using a factor of safety of 1.5 throughout all design strength requirements, in particular in the first instance for all requirements directly connected with the symmetric flight envelope. Alongside this is shown the desirability of changing the flight envelope to agree more nearly, with results obtained in practice (from V-g records).	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The case for factors of safety of 1.5 instead of 2.0, with special reference to the flight envelope	en_US