Print Email Facebook Twitter Engineering property comparisons of 7050-T73651, 7010-T7651 and 7010-T73651 aluminium alloy plate Title Engineering property comparisons of 7050-T73651, 7010-T7651 and 7010-T73651 aluminium alloy plate Author Schra, L. 't Hart, W.G.J. Institution National Aerospace Laboratory NLR Date 1980-12-31 Abstract A comparison of some engineering properties of T050-T73é51, TOIO-TT65I and TOIO-TT365I plate has been made. The properties investigated were strength, stress corrosion resistance, fracture toughness and fatigue crack propagation resistance under flight simulation loading. It was found that both 7050 and 7010 are high strength deep hardenable alloys with only minor differences in crack tolerance properties. The fracture toughness of both alloys is equivalent, while 7050 possesses slightly better resistances to stress corrosion cracking and fatigue crack propagation under flight simulation loading. To reference this document use: http://resolver.tudelft.nl/uuid:d94f1a17-d0c4-4a0b-8d9b-9bb227be6cde Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 80047 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1980 National Aerospace Laboratory NLR Files PDF 80047.pdf 22.05 MB Close viewer /islandora/object/uuid:d94f1a17-d0c4-4a0b-8d9b-9bb227be6cde/datastream/OBJ/view