{"title":"On The Relation between Hardness and Yield Strength in a Sand Cast AZ91 Alloy","authors":"C. L. Bancroft, C. H. Cáceres, J. Griffiths","doi":"10.1002/9781118808962.CH40","DOIUrl":null,"url":null,"abstract":"The effect of ageing time at 165 degrees C on the mechanical properties of sand cast AZ91 alloy has been studied. The hardness, H-upsilon, and 0.2% proof stress, YS, increase with ageing time while the tensile ductility decreases. It is possible to fit the flow curves of the material to the equation sigma = K epsilon(pl)(n), where sigma is the true stress and epsilon(pl) the true plastic strain, with a single K-value (570 MPa) and varying the strain hardening exponent, n, according to the alloy temper. It is shown that the value of n is related to the Vickers hardness number by n = 1.382 - 0.265 In(H-upsilon) and that this expression can be used to calculate the 0.2% proof stress as YS = 569 (0.002)(n) (the value of 569 MPa used here is because the proof stress is the engineering stress).","PeriodicalId":200097,"journal":{"name":"Magnesium Technology","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-10-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Magnesium Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1002/9781118808962.CH40","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
The effect of ageing time at 165 degrees C on the mechanical properties of sand cast AZ91 alloy has been studied. The hardness, H-upsilon, and 0.2% proof stress, YS, increase with ageing time while the tensile ductility decreases. It is possible to fit the flow curves of the material to the equation sigma = K epsilon(pl)(n), where sigma is the true stress and epsilon(pl) the true plastic strain, with a single K-value (570 MPa) and varying the strain hardening exponent, n, according to the alloy temper. It is shown that the value of n is related to the Vickers hardness number by n = 1.382 - 0.265 In(H-upsilon) and that this expression can be used to calculate the 0.2% proof stress as YS = 569 (0.002)(n) (the value of 569 MPa used here is because the proof stress is the engineering stress).