Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly...

 

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Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib). Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib). Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib). Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib). Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib). Heat treatment of the alloy in the design applica- tion of Problem 6.4 does not significantly affect the modulus of elasticity, but does change strength and ductility. For a particular heat treatment, the corre- sponding mechanical property data are Y.S. = 1,000 MPa (145 ksi), %3D T.S. = 1,380 MPa (200 ksi), %3D and % clongation at failure = 12. Again, considering a 20-mm-diameter by 1-m-long bar of this alloy, what is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Here is problem 6.4 as referenced in the above question. DO NOT compete the below question Consider the 1040 carbon steel listed in Table 6.1. (a) A 20-mm-diameter bar of this alloy is used as a structural member in an engineering design. The unstressed length of the bar is precisely 1 m. The structural load on the bar is 1.2 x 10° N in tension. What will be the length of the bar under this struc- tural load? (b) A design engineer is considering a structural change that will increase the tensile load on this member. What is the maximum tensile load that can be permitted without producing extensive plastic deformation of the bar? Give your answers in both newtons (N) and pounds force (Ib).

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