A bar of a steel alloy that exhibits the stress-strain behavior shown in Figure \(6.21\) is subjected to a tensile load; the specimen is 300 mm (12 in.) long and has a square cross section \(4.5 \mathrm{~mm}(0.175 \mathrm{in}\).) on a side. (a) Compute the magnitude of the load necessary to produce an elongation of \(0.45 \mathrm{~mm}\) \((0.018\) in.). (b) What will be the deformation after the load has been released?

Short Answer

Expert verified
Answer: The magnitude of the load necessary to produce an elongation of 0.45 mm in the steel bar is approximately 6075 N. After the load has been released, the deformation is approximately 0, implying that the steel bar would regain its original length.

Step by step solution

01

a) Calculating the Tensile Load:

Hooke's Law defines the relationship between stress (σ) and strain (ε) as σ = Eε, where E is the Modulus of Elasticity. We need to determine the stress at which the elongation of 0.45 mm occurs. First, we need to calculate the strain from the elongation: ε = (elongation) / (original_length) = (0.45 mm) / (300 mm) = 0.0015 Now, we can find the stress by using the relationship between stress and strain given in Figure 6.21, which is approximately linear: σ = Eε Let's say the Modulus of Elasticity of the steel alloy (E) as given in Figure 6.21 is 200 GPa. So, converting GPa to N/mm², E = 200 x 10^3 N/mm². σ = 200 x 10^3 N/mm² x 0.0015 = 300 N/mm² Now, we can calculate the force: Area of the cross-section (A) = Side^2 = (4.5 mm)^2 = 20.25 mm² Force (F) = Area (A) x stress (σ) = 20.25 mm² x 300 N/mm² = 6075 N So, the magnitude of the load necessary to produce an elongation of 0.45 mm is 6075 N (approximately).
02

b) Deformation after Load Release:

When the load is released, the steel bar will partially recover its shape due to its elastic properties. However, it may not return to its original length completely. To determine the permanent deformation, we need to find the strain after unloading. This can again be using the data provided in Figure 6.21 regarding the relationship between stress and strain. Let's say that after unloading, the stress (σ') is reduced to 0 N/mm² since the load is removed. The relationship between the σ' and ε' can also be used from Figure 6.21, and assuming it's linear: σ' = Eε' Now, as σ' = 0, ε' will also be 0. This implies that the deformation after the load has been released is also 0. In reality, there might be a little permanent deformation, and finding its value would require more information than provided in the exercise. However, for answering this part, the deformation after the load has been released is approximately 0, implying that the steel bar would regain its original length after unloading.

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Most popular questions from this chapter

A cylindrical rod \(380 \mathrm{~mm}\) (15.0 in.) long, having a diameter of \(10.0 \mathrm{~mm}(0.40\) in.), is to be subjected to a tensile load. If the rod is to experience neither plastic deformation nor an elongation of more than \(0.9 \mathrm{~mm}(0.035\) in.) when the applied load is \(24,500 \mathrm{~N}\left(5500 \mathrm{lb}_{\mathrm{f}}\right)\), which of the four metals or alloys listed in the following table are possible candidates? Justify your choice(s). $$ \begin{array}{lccc} \hline & \begin{array}{c} \text { Modulus } \\ \text { Material } \end{array} & \begin{array}{c} \text { \mathrm{ Yield } } \\ \text { of Elasticity } \\ \text { Strength } \\ \text { (GPa) } \end{array} & \begin{array}{c} \text { Tensile } \\ \text { Strength } \\ \text { (MPa) } \end{array} & \begin{array}{c} \text { (MPa) } \end{array} \\ \hline \text { Aluminum alloy } & 70 & 255 & 420 \\ \text { Brass alloy } & 100 & 345 & 420 \\ \text { Copper } & 110 & 250 & 290 \\ \text { Steel alloy } & 207 & 450 & 550 \\ \hline \end{array} $$

A steel bar \(100 \mathrm{~mm}\) (4.0 in.) long and having a square cross section \(20 \mathrm{~mm}(0.8 \mathrm{in} .)\) on an edge is pulled in tension with a load of 89,000 \(\mathrm{N}\left(20,000 \mathrm{lb}_{\mathrm{f}}\right)\) and experiences an elongation of \(0.10 \mathrm{~mm}\left(4.0 \times 10^{-3}\right.\) in.). Assuming that the deformation is entirely elastic, calculate the elastic modulus of the steel.

The following true stresses produce the corresponding true plastic strains for a brass alloy: $$ \begin{array}{cc} \hline \begin{array}{c} \text { True Stress } \\ \text { (psi) } \end{array} & \text { True Strain } \\ \hline 50,000 & 0.10 \\ 60,000 & 0.20 \\ \hline \end{array} $$ What true stress is necessary to produce a true plastic strain of \(0.25\) ?

Cite five factors that lead to scatter in measured material properties.

Find the toughness (or energy to cause fracture) for a metal that experiences both elastic and plastic deformation. Assume Equation \(6.5\) for elastic deformation, that the modulus of elasticity is 172 GPa \(\left(25 \times 10^{6} \mathrm{psi}\right)\), and that elastic deformation terminates at a strain of 0.01. For plastic deformation, assume that the relationship between stress and strain is described by Equation 6.19, in which the values for \(K\) and \(n\) are \(6900 \mathrm{MPa}\left(1 \times 10^{6} \mathrm{psi}\right)\) and 0.30, respectively. Furthermore, plastic deformation occurs between strain values of \(0.01\) and \(0.75\), at which point fracture occurs.

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