x =9
y = 0
- Q4 Please Detailed And Full Calculation And Clear Writting X 9 Y 0 1 (7.78 KiB) Viewed 34 times
- Q4 Please Detailed And Full Calculation And Clear Writting X 9 Y 0 2 (55.29 KiB) Viewed 34 times
4) A cylindrical specimen of aluminum having a diameter of (0.1*(12+XY)) mm and a gauge length of 50.800 mm is pulled in tension. Use the load-elongation characteristics shown in the following table to complete parts (a) through (f). (a) Plot the data as engineering stress versus engineering strain. (b) Compute the modulus of elasticity. (c) Determine the yield strength at a strain offset of 0.002. (d) Determine the tensile strength of this alloy. (e) What is the approximate ductility, in percent elongation? (f) Compute the modulus of resilience. Load N 0 7,330 15.100 23.100 30,400 34,400 38,400 41,300 44.800 46.200 47.300 47.500 46,100 44,800 42,600 36,400 Length lbs mm in. 0 50.800 2.000 1,650 50.851 2.002 3.400 50.902 2.004 5.200 50.952 2.006 6,850 51.003 2.008 7,750 51.054 2.010 8,650 51.308 2.020 9,300 51.816 2.040 10,100 52.832 2.080 10,400 53.848 2.120 10,650 54.864 2.160 10,700 55.880 2.200 10,400 56.896 2.240 10,100 57.658 2.270 9,600 58.420 2.300 8.200 59.182 2.330 Fracture