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In machining of parts for the aircraft industry, residual stresses are ones of the most specified customer requirements. This paper utilizes modelling analysis to predict residual stresses values for variety of cutting conditions in finish turning of the aircraft steel AISI 9310. Taguchi method and ANOVA analysis were used to determine if the independent variables like flank wear VB and feed f are related to the components of the residual stresses, and to explore the forms of these relationships.

Predictive Modelling of the Residual Stresses Distribution in the Aircraft Steel Part After Machining