Q2 :A specimen of ductile cast iron having a rectangular cross sectionof dimensions 4.8 mm * 15.9 mm (3/16 in. 5/8 in.) is deformed intension. Using the load-elongation data tabulated below, completeproblems (a) through (f).LoadLengthIbin.75.0002.9532.9544,7401,0652,0552,9003,72075.0259,14075.0502.95512,92075.0752.95616,54075.1132.95718,30075.1504.1104,5305,1452.95920,17075.2252.96222,90075.3752.96825,0705,63575.5252.97326,8006,02575.7502.98228,64030,24031,10076.50078.00079.5006,4403.0123.0716,8007,0007,0306,9303.13031,28081.0003.18930,82082.5003.24884.0003.30729,18027,1906,5606,11085.50087.00088.725Freeture3.3663.4255,4304,26524,14018,9703.493a) 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) Compute the modulus of resilience.f) What is the ductility, in percent elongation?

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Q2 :A specimen of ductile cast iron having a rectangular cross section of dimensions 4.8 mm 15.9 mm (3/16 in. 5/8 in.) is deformed in tension. Using the load-elongation data tabulated below, complete problems (a) through (f). Load Length in 2.953 75.000 4,740 9,140 12,920 16,540 75.025 1,065 2,055 2,900 2.954 75,050 2.955 75.075 2.956 3,720 75.113 2.957 18,300 4,110 75.150 2.959 20,170 75.225 75.375 4,530 2.962 22,900 2.968 5,145 5,635 6,025 25,070 75.525 2.973 75.750 2.982 26,800 28,640 6,440 76.500 3.012 78.000 3.071 30,240 31,100 31,280 6,800 7,000 7,030 6,930 79.500 3.130 81.000 82.500 3.189 3.248 3.307 30,820 84.000 85.500 29,180 6,560 6,110 5,430 4,265 Fracture 27,190 3.366 24,140 87.000 3.425 18,970 88.725 3.493 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) Compute the modulus of resilience. f) What is the ductility, in percent elongation?

Q2 :A specimen of ductile cast iron having a rectangular cross section of dimensions 4.8 mm 15.9 mm (3/16 in. 5/8 in.) is deformed in tension. Using the load-elongation data tabulated below, complete problems (a) through (f). Load Length in 2.953 75.000 4,740 9,140 12,920 16,540 75.025 1,065 2,055 2,900 2.954 75,050 2.955 75.075 2.956 3,720 75.113 2.957 18,300 4,110 75.150 2.959 20,170 75.225 75.375 4,530 2.962 22,900 2.968 5,145 5,635 6,025 25,070 75.525 2.973 75.750 2.982 26,800 28,640 6,440 76.500 3.012 78.000 3.071 30,240 31,100 31,280 6,800 7,000 7,030 6,930 79.500 3.130 81.000 82.500 3.189 3.248 3.307 30,820 84.000 85.500 29,180 6,560 6,110 5,430 4,265 Fracture 27,190 3.366 24,140 87.000 3.425 18,970 88.725 3.493 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) Compute the modulus of resilience. f) What is the ductility, in percent elongation?

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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