z-logo
open-access-imgOpen Access
Predictive Modelling of the Residual Stresses Distribution in the Aircraft Steel Part After Machining
Author(s) -
Wojciech Zębala,
Grzegorz Struzikiewicz,
Ksenia Rumian
Publication year - 2016
Publication title -
the publications of the multiscience - xxx. microcad international scientific conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.26649/musci.2016.068
Subject(s) - residual stress , machining , residual , computer science , distribution (mathematics) , engineering , mechanical engineering , materials science , metallurgy , mathematics , algorithm , mathematical analysis
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.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom