mighoser
Aerospace
- Jul 10, 2006
- 160
Besides hardness is there a method to determine heat treat condition (in parts) besides hardness testing. From what I've read, The TH and RH grades are easy to segregate from microstructure (TH = cat's and dog's). How about between different Aging temperatures (TH 950, 1000, 1050, 1075, 1100)? What would the result of processing Condition C material to the TH1050 process (ie start with condition C instead of A)?