Print Email Facebook Twitter Engineering property comparisons of the aluminium plate alloys 7050-T7365I, 7010-T7365I and 7010-T765I Title Engineering property comparisons of the aluminium plate alloys 7050-T7365I, 7010-T7365I and 7010-T765I Author 't Hart, W.G.J. Schra, L. Institution National Aerospace Laboratory NLR Date 1980-11-30 Abstract The Al-Zn-Mg-Cu alloy 7050 produced by Alcoa is a typical plate and forging alloy because of its low quench sensitivity. In order to compare this alloy with the earlier tested plate alloy 7010 an experimental programme was performed involving tensile, fracture toughness, and fatigue testing. In addition stress corrosion crack initiation and stress corrosion crack growth tests were executed Subject Aluminum alloysMechanical propertiesMetal platesForgingsCrack propagationFracture strengthFatigue testsTensile testsStress corrosion crackingCrack initiationMicro structureFlight simulationGust loadsProcedures To reference this document use: http://resolver.tudelft.nl/uuid:0d88ca62-498a-4533-a339-4d07664d62a3 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 80108 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1980 National Aerospace Laboratory NLR Files PDF NLR_TR_80108_U.pdf 17.32 MB Close viewer /islandora/object/uuid:0d88ca62-498a-4533-a339-4d07664d62a3/datastream/OBJ/view