ALUMINUM - Materials for Civil and Construction Engineers - page 150

T ABLE 4.4 (Continued)

5005 O 18 124 6 41 25 28 11 76 0.8 Mg

H-12 20 138 19 131 10 14 97

H-14 23 159 22 152 6 14 97

H-16 26 179 25 172 5 15 103

H-18 29 200 28 193 4 16 110

H-32 20 138 17 117 11 36 14 97

H-34 23 159 20 138 8 41 14 97

H-36 26 179 24 165 6 46 15 103

H-38 29 200 27 186 5 51 16 110

5086 O 38 262 17 117 22 30 60 23 159 21 145 Mg

H-32 42 290 30 207 12 16 72 25 172 22 152 0.45 Mn

H-34 47 324 37 255 10 14 82 27 186 23 159

H-111 40 276 27 186 17 65 23 159 21 145

H-112 39 269 19 131 14 64 23 159 21 145

H-116 42 290 30 207 16 72 25 173 22 152

5456 O 45 310 23 159 20 24 70 27 186 22 152 5.1Mg

H-111 47 324 33 228 18 75 27 186 24 165 0.7Mn

H-112 45 310 24 156 22 70 27 186 0.12 Cr

H-116 51 352 37 255 16 90 30 207 23 159

1

percent elongation over 2 in.
Brinell number, 500-kg load
500,000,000 cycles of complete stress reversal using R.R. Moore type of machine and specimen.

2

3