Tensile Properties of a Hot Stretch Formed Ti-6Al-4V Alloy Component for Aerospace Applications
Author:
Publisher
Jan Evangelista Purkyne University in Usti nad Labem
Subject
Industrial and Manufacturing Engineering
Link
http://journalmt.com/doi/10.21062/ujep/x.2017/a/1213-2489/MT/17/2/141.pdf
Reference16 articles.
1. Process parameters optimization of Ti-6Al-4V alloy sheet during hot stretch-creep forming
2. Titanium Hot Stretch Forming: Experimental and Modeling Residual Stress Analysis
3. Hot Stretch Forming of a Titanium Alloy Component for Aeronautic: Mechanical and Modeling
4. Microstructure of a Hot Forged Ti 5-5-5-3 Aeronautical Component
5. A study on springback of profile plane stretch–bending in the loading method of pretension and moment
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