Hi, I am looking at Aluminum 4032-T6 and 4032-T651. From what I understand, both processes are the same with the exception of stretching process for the T651. Since the material is stressed by 1-3%, would that affect the yield strength and/or ultimate strength of the material?
How do we know when stress relief is required and how much stretching is required?
How do we know when stress relief is required and how much stretching is required?
