[1] Lu K. The Future of Metals. Science, 2010, 328: 319-320.
[2] 张鹏省，毛小南，韩栋. 航空航天用钛合金盘件开发与应用. 钛工业进展，2011, 28(3): 6-8.
[3] 张利军，常辉，薛祥义. 等温锻造技术及其在航空工业中的应用. 热加工工艺，2010，39(21): 21-24.
[4] 张涛，李琦，何露. TC2钛合金异形件热成形工艺研究. 航空制造技术，2011(16)：57-59.
[5] 辛社伟，赵永庆. 关于钛合金的热处理和析出相的讨论. 金属热处理，2006(31)：39-42.
[6] 李瑞婷，郭伟，朱颖. Tc4钛合金超塑成形研究现状及其发展展望. 航空制造技术，2012, 15: 91-99.
[7] Sellars C M, Tegart W J, Mc G. La relation entre la résistance et la structure dans la déformation à chaud. Memoires Scientific Rev. Métallurg, 1966, 9: 731-746.
[8] Ma F, Lu W, Qin J J. Microstructure evolution of near-αtitanium alloys during thermomechanical processing. Materials Science and Engineering A, 2006, 416: 59-65.
[9] Salem A A, Semiatin S L. Anisotropy of the hot plastic deformation of Ti-6Al-4V single-colony samples. Materials Science and Engineering: A, 2009, 508: 114-120.
[10] Sargent G A, Zane A P, Fagin P N, et al. Low-temperature coarsening and plastic flow behavior of an alpha/beta titanium billet material with an ultrafine microstructure. Metallurgical and Materials Transactions A: Physical Metallurgy and Materials Science, 2008, 39: 2949-2964.
[11] McQueen H J, Ryan N D. Constitutive analysis in hot working. Materials Science and Engineering A, 2002, 322: 43-63.
2013, 
