Kacar, IlyasKilic, Suleyman2024-11-072024-11-0720221300-18841304-4915https://doi.org/10.17341/gazimmfd.654200https://search.trdizin.gov.tr/tr/yayin/detay/508754https://hdl.handle.net/11480/14725In this study, plasticity models have been developed to be used in cold forging simulations of AA7075-T6 alloy which is widely used in aviation industry. In addition, the coefficients of the obtained models have been calibrated using genetic algorithm optimization method. As the hardening rule in models; bilinear isotropic is combined with Chaboche's nonlinear kinematic hardening rule (three-termed). Plasticity models have been obtained by using the associated flow rule and Hill48 yield criterion in addition to the hardening rules. Experimental stress values have been compared with those obtained from the models. As a result, the most suitable hardening model for monotonic/cyclic loading deformation conditions is presented and the effects of the model parameters on the simulation results are shown.eninfo:eu-repo/semantics/openAccessChaboche kinematic hardening modelbilinear isotropic hardening modelgenetic algorithmAA7075-T6cold forgingParameter determination and calibration of the combined plasticity model through inverse analysis for cold forging simulation of 7075-T6 aluminum alloy7075-T6 alüminyum alaşiminin so?uk dövme simülasyonu için birleşik plastisite model parametrelerinin tespiti ve tersine analiz ile kalibrasyonuArticle3742091210410.17341/gazimmfd.6542002-s2.0-85128710108Q2508754WOS:000767316300026Q4