This table contains mechanical property reference data for aluminum and its alloys.
This table includes Temper, Yield strength, Tensile strength, Shear Modulus of Rupture, Elongation, Fatigue Strength and Brinnel hardness information.
(Tabulated in accordance with the Unified Numbering System for Metals and Alloys (UNS), Society of Automotive Engineers, Warrendale, Pa., 1975. This reference contains the cross reference numbers for AISI, ASTM, FED, MIL SPEC, and SAE specifications. These are typical properties for sizes of about 1/2 inch. A typical value may be neither the mean nor the minimum. It is a value which can be obtained when the purchase specifications are carefully written and with continuous inspection and testing. The values given for fatigue strength, S_f, correspond to 50e7 cycles of completely reversed stress. Aluminum alloys do not have an endurance limit. The yield strength is 0.2% offset value. Multiply strength in kpsi by 6.89 to get strength in MPa.)
UNS Yield Tensile Shear modulus Fatigue Elongation Brinell alloy strength, strength, of rupture, strength, in 2 in, hardness, number Temper kpsi kpsi kpsi kpsi % H_b ------ ------- --------- --------- ------------- --------- ---------- --------- A91100 -O 5 13 9.5 5 45 23 A91100 -H12 14 15.5 10 6 25 28 A91100 -H14 20 22 14 9 16 40 A91100 -H16 24 26 15 9.5 14 47 A91100 -H18 27 29 16 10 10 55 A93003 -O 6 16 11 7 40 28 A93003 -H12 17 19 12 8 20 35 A93003 -H14 20 22 14 9 16 40 A93003 -H16 24 26 15 9.5 14 47 A93003 -H18 27 29 16 10 10 55 A93004 -O 10 26 16 14 25 45 A93004 -H32 22 31 17 14.5 17 52 A93004 -H34 27 34 18 15 12 63 A93004 -H36 31 37 20 15.5 9 70 A93004 -H38 34 40 21 16 6 77 A92011 -T3 48 55 32 18 15 95 A92011 -T8 45 59 35 18 12 100 A92014 -O 14 27 18 13 18 45 A92014 -T4 40 62 38 20 20 105 A92014 -T6 60 70 42 18 13 135 A92017 -O 10 26 18 13 22 45 A92017 -T4 40 62 38 18 22 105 A92018 -T61 46 61 39 17 12 120 A92024 -O 11 27 18 13 22 47 A92024 -T3 50 70 41 20 16 120 A92024 -T4 48 68 41 20 19 120 A92024 -T36 57 73 42 18 13 130 A95052 -O 13 28 18 17 30 45 A95052 -H32 27 34 20 17.5 18 62 A95052 -H34 31 37 21 18 14 67 A95052 -H36 34 39 23 18.5 10 74 A95052 -H38 36 41 24 19 8 85 A95056 -O 22 42 26 20 35 A95056 -H18 59 63 34 22 10 A95056 -H38 50 60 32 22 15 A96061 -O 8 18 12.5 9 30 30 A96061 -T4 21 35 24 13.5 25 65 A96061 -T6 40 45 30 13.5 17 95 A97075 -T6 72 82 49 24 11 150 ------ ------- --------- --------- ------------- --------- ---------- ---------Shigley, Mechanical Engineering Design, 1980, McGraw Hill