Home   |   About Journal   |   Editorial Board   |   Instruction   |   Publication Ethics Statement   |   Subscriptions   |   Contacts Us   |   Chinese
Aeronautical Manufacturing Technology  2016, Issue (23/24): 36-41    DOI: 10.16080/j.issn1671-833x.2016.23/24.036
FORUM Current Issue | Archive | Adv Search |
High Temperature Stress-Rupture Properties of TiAl Base Alloy Directionally Solidified by Cold Crucible Method
DING Hongsheng1, LI Jintao1, WANG Qiang1, GENG Hongbin2, CHEN Ruirun1,GUO Jingjie1, FU Hengzhi1
(1. National Key Laboratory for Precision Hot Processing of Metals, Harbin Institute of Technology, Harbin 150001, China;
2. National Defense Science and Technology Key Lab for Space Materials Behavior and Evaluation,
Harbin Institute of Technology, Harbin 150001, China)
Copyright © Editorial Board of Aeronautical Manufacturing Technology
Supported by: Beijing Magtech