The resistance of aluminium and beryllium bronzes to fatigue and corrosion-fatigue

dc.contributor.author	D. G. Sopwith	en_US
dc.date.accessioned	2014-10-21T15:54:23Z
dc.date.available	2014-10-21T15:54:23Z
dc.date.issued	1940	en_US
dc.identifier.other	ARC/R&M-2486	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3643
dc.description.abstract	The investigation of the fatigue and corrosion-fatigue resistance of special bronzes (Gough and Sopwith, 1937) is extended to include (1) aluminium bronze (D.T.D.I60), (2) beryllium bronze (2.25 per cent. Be), each in two heat-treated conditions. In neither material is the fatigue or corrosion-fatigue resistance appreciably higher in the heat-treated condition than in the condition as received. The fatigue strength in air of the beryllium bronze is almost independent of the ultimate stress, which varied from 32 to 81 ton/in.².	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The resistance of aluminium and beryllium bronzes to fatigue and corrosion-fatigue	en_US