Microstructure study and constitutive modeling of Ti-6Al-4V alloy at elevated temperatures

被引:119
|
作者
Kotkunde, Nitin [1 ]
Krishnamurthy, Hansoge Nitin [1 ]
Puranik, Pavan [1 ]
Gupta, Amit Kumar [1 ]
Singh, Swadesh Kumar [2 ]
机构
[1] BITS Pilani, Dept Mech Engn, Hyderabad 500078, Andhra Pradesh, India
[2] GRIET, Dept Mech Engn, Hyderabad 500072, AP, India
关键词
STRAIN-AGING REGIME; STAINLESS-STEEL; 316; FLOW-STRESS; TITANIUM-ALLOYS; BEHAVIOR; RATES;
D O I
10.1016/j.matdes.2013.08.006
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A reliable and accurate prediction of flow behavior of metals in industrial forming process considering the coupled effects of strain, strain rate and temperature is crucial in understanding the workability of the metal and optimizing parameters for hot forming process. In this study, the tensile fracture behavior of the Ti-6Al-4V alloy is examined with scanning electron microscope (SEM) over the range of magnifications. SEM study revealed that microvoids and shallow dimples are observed at the fracture surface which indicates the fracture is predominately ductile in nature. Also, an investigation on flow behavior of Ti-6Al-4V alloy is done using constitutive models. Four constitutive models; modified Johnson-Cook (m-JC), modified Arrhenius type equations (m-Arr), modified Zerilli-Armstrong (m-ZA) and Rusinek-Klepaczko (RK) models are developed to predict the flow stress. The predictions of these constitutive models are compared with each other using statistical measures like correlation coefficient, average absolute error and its standard deviation. Comparing the statistical measures, m-Arr model is a better model for predicting the flow stress, but considering the fact that m-ZA model is a physical based model, m-ZA model is preferred over the m-Arr model. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:96 / 103
页数:8
相关论文
共 50 条
  • [1] Comparative study of constitutive modeling for Ti-6Al-4V alloy at low strain rates and elevated temperatures
    Kotkunde, Nitin
    Deole, Aditya D.
    Gupta, Amit Kumar
    Singh, Swadesh Kumar
    MATERIALS & DESIGN, 2014, 55 : 999 - 1005
  • [2] Modeling of flow behavior of Ti-6Al-4V alloy at elevated temperatures
    Porntadawit, J.
    Uthaisangsuk, V.
    Choungthong, P.
    MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2014, 599 : 212 - 222
  • [3] Microstructure and texture of Ti-6Al-4V alloy deformed by rotary forging at elevated temperatures
    Jiang, Shan
    INTERNATIONAL JOURNAL OF MATERIALS RESEARCH, 2020, 111 (10) : 807 - 813
  • [4] Microstructure of Ti-6Al-4V alloy
    Kim, Tae Wan
    Yoon, Yo Han
    Oh, Ho Ra
    Park, Jong Bum
    Lee, Jung-Il
    Ryu, Jeong Ho
    JOURNAL OF THE KOREAN CRYSTAL GROWTH AND CRYSTAL TECHNOLOGY, 2016, 26 (03): : 126 - 130
  • [5] Development of Predictive Models for Formability Study of Ti-6Al-4V alloy at Elevated Temperatures
    Kotkunde, Nitin
    Balu, Aditya
    Gupta, Amit Kumar
    Singh, Swadesh Kumar
    MATERIALS TODAY-PROCEEDINGS, 2017, 4 (02) : 937 - 945
  • [6] A Study on Yield Function for Ti-6Al-4V Titanium Alloy Sheets at Elevated Temperatures
    Duc-Toan Nguyen
    Park, Jin-Gee
    Kim, Young-Suk
    TRANSACTIONS OF THE INDIAN INSTITUTE OF METALS, 2016, 69 (07) : 1343 - 1350
  • [7] Superplasticity of Ti-6Al-4V Titanium Alloy: Microstructure Evolution and Constitutive Modelling
    Mosleh, Ahmed O.
    Mikhaylovskaya, Anastasia V.
    Kotov, Anton D.
    Kwame, James S.
    Aksenov, Sergey A.
    MATERIALS, 2019, 12 (11)
  • [8] Investigation of the constitutive relationship and formability of Ti-6Al-4V alloy considering anisotropy and mesoscopic damage at elevated temperatures
    Gao, Song
    Wang, Guotao
    Sun, Yingli
    Li, Qihan
    Hao, Zhaopeng
    Li, Hui
    JOURNAL OF ALLOYS AND COMPOUNDS, 2025, 1022
  • [9] High cycle fatigue behaviour of Ti-6Al-4V alloy at elevated temperatures
    Tokaji, K
    SCRIPTA MATERIALIA, 2006, 54 (12) : 2143 - 2148
  • [10] New constitutive relationship for Ti-6Al-4V alloy
    Nie, L., 2001, Chinese Journal of Aeronautics (21):