Downloaded from https://www.everyspec.com STRUCTURES sFit wt , !- TITANIUM ALLOY SI , _ 5%A 1, 2.5% Sn Figure 2-8. Effect of Toemperaure 4 - - on Cost-Strength Ratio for Several Typical Materials MAGNES!UM ALLOY AZ31A U-ALUMiNUM ALLOY 2024 -T6 Figuic -2-9. Compressive S E Stress-Strain .;.,es for IR.ONEL X ]STAINLESS STEEL 2024-T3 Aluminum Atir' 0[ #A~~ -A30 Clad Sheet Stock at S 0 oo 8 0 1200 1606 2000 Various Temperalure3 TEMPERATURE , F 50 STR~AN RATE0.002/MiN.- .004 0.002 /min strain Woe 2 . .0 -- - I/?- HOUR AT TEST TEMPERATURE 0 -. o0*. 0.0018 Emj*t The strain at rf,500 psi and 250OF is 0.0018 ISSTRAIN( 28