z-logo
Premium
Effect of Strain Rate on the Hot Ductility Behavior of a Continuously Cast Ti–Nb Microalloyed Steel
Author(s) -
Gontijo Marina,
Hoflehner Christian,
Estermann Paul,
Ilie Sergiu,
Six Jakob,
Sommitsch Christof
Publication year - 2020
Publication title -
steel research international
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.603
H-Index - 49
eISSN - 1869-344X
pISSN - 1611-3683
DOI - 10.1002/srin.202000222
Subject(s) - materials science , ductility (earth science) , microalloyed steel , metallurgy , strain rate , microstructure , continuous casting , precipitation , tensile testing , ultimate tensile strength , vacuum induction melting , casting , composite material , creep , austenite , physics , meteorology
During the continuous casting process, alloys may be more susceptible to crack initiation under some conditions due to lower ductility. A Ti–Nb microalloyed steel is subjected to in situ melted hot tensile tests to evaluate its hot ductility behavior. The ductility is examined at different strain rates and temperatures. The samples are heated with an induction coil to the melting temperature in a vacuum atmosphere. Afterward, they are cooled to the desired test temperatures. Hot tensile tests are conducted by a thermomechanical simulator with strain rates varying from 10 −5 to 10 −2  s −1 . The results show a ductility minimum around 800 °C for the standard strain rate of 10 −3  s −1 and a significant influence of the changes in strain rate in the behavior of the alloy for all the tested temperatures. The fracture surfaces are compared for 700, 800, and 900 °C at 10 −4 , 10 −3 , and 10 −2  s −1 , as well as the microstructure. Computer simulations are done for the determination of the transformation temperatures, Scheil–Gulliver solidification simulation, and analysis of the precipitation kinetics during the tests. The results from simulations are discussed in comparison with the ones seen experimentally.

This content is not available in your region!

Continue researching here.

Having issues? You can contact us here