2004
DOI: 10.4028/www.scientific.net/msf.449-452.189
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Prediction of Microstructure During High Temperature Forming of Ti-6Al-4V Alloy

Abstract: Prediction of final microstructures after high temperature forming of Ti-6Al-4V alloy was´attempted in this study. Using two typical microstructures, i.e., equiaxed and Widmanstätten microstructures, compression test was carried out up to the strain level of 0.6 at various temperatures (700 ~ 1100°C) and strain rates (10-4 ~ 102/s). From the flow stress-strain data, parameters such as strain rate sensitivity (m) and activation energy (Q) were calculated and used to establish constitutive equations for both mic… Show more

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Cited by 3 publications
(2 citation statements)
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“…In general, the chilling effect is attributed to the temperature difference between the hot workpiece and cold die in non-isothermal bulk forming processes. Because of the chilling of the workpiece in contact with the cold die, a flow stress deviation between the surface and the inside of the heated workpiece occurs, and this deviation leads to the formation of defects such as laps, flow-through defects, cracking, and other flow instabilities [1][2][3][4]. The amount and extent of the chilling can be determined as functions of interface heat transfer, friction, deformation rate, and initial temperature difference between workpiece and die.…”
Section: Introductionmentioning
confidence: 99%
“…In general, the chilling effect is attributed to the temperature difference between the hot workpiece and cold die in non-isothermal bulk forming processes. Because of the chilling of the workpiece in contact with the cold die, a flow stress deviation between the surface and the inside of the heated workpiece occurs, and this deviation leads to the formation of defects such as laps, flow-through defects, cracking, and other flow instabilities [1][2][3][4]. The amount and extent of the chilling can be determined as functions of interface heat transfer, friction, deformation rate, and initial temperature difference between workpiece and die.…”
Section: Introductionmentioning
confidence: 99%
“…Ti-6Al-4V alloy has been widely used for aerospace applications because of its good specific strength at elevated temperatures and its excellent corrosion *Corresponding author: Department of Materials Science and Engineering, Pohang University of Science and Technology, San 31, Hyoja-dong, Nam-gu, Pohang, Gyungbuk 790-784, Republic of Korea. email: cslee@postech.ac.kr resistance [7][8][9][10]. However, despite its excellent mechanical and chemical properties, the processing window for high-temperature forming is rather narrow, often making it difficult to form final products that are free from defects.…”
Section: Introductionmentioning
confidence: 99%