For a bronze alloy, the stress at which plastic deformation begins is \(275 \mathrm{MPa}\) (40,000 psi), and the modulus of elasticity is \(115 \mathrm{GPa}\) \(\left(16.7 \times 10^{6} \mathrm{psi}\right) .\) (a) What is the maximum load that may be applied to a specimen with a cross- sectional area of \(325 \mathrm{~mm}^{2}\left(0.5 \mathrm{in} .^{2}\right)\) without plastic deformation? (b) If the original specimen length is \(115 \mathrm{~mm}\) (4.5 in.), what is the maximum length to which it may be stretched without causing plastic deformation?

Short Answer

Expert verified
Answer: The maximum load that the bronze alloy specimen can withstand without causing plastic deformation is 89,375 N. The maximum length it can be stretched without causing plastic deformation is approximately 115.275 mm (4.534 inches).

Step by step solution

01

(a) Calculate the maximum load

To calculate the maximum load that can be applied to the specimen without causing plastic deformation, we can use the formula for stress: Stress = Force / Area From the given values, the stress at which plastic deformation begins is 275 MPa and the cross-sectional area of the specimen is 325 mm². Rearrange the formula to get: Force = Stress × Area Substitute the given values: Force = 275 MPa × 325 mm² Now we can convert MPa to N/mm², so 1 MPa = 1 N/mm²: Force = 275 N/mm² × 325 mm² Calculate the Force: Force = 89375 N So, the maximum load that may be applied to the specimen without causing plastic deformation is 89,375 N.
02

(b) Calculate the maximum length

To find the maximum length the specimen can be stretched without causing plastic deformation, we need to first calculate the strain. The strain can be found using the following formula: Strain = Stress / Modulus of Elasticity Substitute the given values: Strain = (275 MPa) / 115 GPa Convert the units so that both stress and modulus of elasticity have the same units (in this case, GPa). 1 MPa = 0.001 GPa: Strain = (0.275 GPa) / 115 GPa Calculate the Strain: Strain ≈ 0.002391 Now, we can calculate the change in length by multiplying the Strain by the original length: Change in length = Strain × Original_length Substitute the given value for original length (115 mm): Change in length = 0.002391 × 115 mm Calculate the change in length: Change in length ≈ 0.275 mm So, the change in length without causing plastic deformation is approximately 0.275 mm. Now, we will add this change in length to the original length to find the maximum length the specimen can be stretched without causing plastic deformation: Maximum_length = Original_length + Change_Length Maximum_length = 115 mm + 0.275 mm ≈ 115.275 mm Therefore, the maximum length to which the specimen may be stretched without causing plastic deformation is approximately 115.275 mm (4.534 inches).

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Most popular questions from this chapter

A brass alloy is known to have a yield strength of \(275 \mathrm{MPa}(40,000 \mathrm{psi})\), a tensile strength of \(380 \mathrm{MPa}(55,000 \mathrm{psi})\), and an elastic modulus of \(103 \mathrm{GPa}\left(15.0 \times 10^{6} \mathrm{psi}\right)\). A cylindrical specimen of this alloy \(12.7 \mathrm{~mm}(0.50\) in.) in diameter and \(250 \mathrm{~mm}\) (10.0 in.) long is stressed in tension and found to elongate \(7.6 \mathrm{~mm}(0.30 \mathrm{in}\).). On the basis of the information given, is it possible to compute the magnitude of the load that is necessary to produce this change in length? If so, calculate the load. If not, explain why.

A cylindrical specimen of a hypothetical metal alloy is stressed in compression. If its original and final diameters are \(20.000\) and \(20.025 \mathrm{~mm}\), respectively, and its final length is \(74.96 \mathrm{~mm}\), compute its original length if the deformation is totally elastic. The elastic and shear moduli for this alloy are \(105 \mathrm{GPa}\) and \(39.7 \mathrm{GPa}\), respectively.

A cylindrical metal specimen having an original diameter of \(12.8 \mathrm{~mm}(0.505\) in.) and gauge length of \(50.80 \mathrm{~mm}(2.000 \mathrm{in} .)\) is pulled in tension until fracture occurs. The diameter at the point of fracture is \(6.60 \mathrm{~mm}(0.260 \mathrm{in} .)\), and the fractured gauge length is \(72.14 \mathrm{~mm}\) (2.840 in.). Calculate the ductility in terms of percent reduction in area and percent elongation.

Using the data in Problem \(6.29\) and Equations 6.15, 6.16, and 6.18a, generate a true stress-true strain plot for aluminum. Equation \(6.18\) a becomes invalid past the point at which necking begins; therefore, measured diameters are given in the following table for the last four data points, which should be used in true stress computations. $$ \begin{array}{cccccc} \hline \text {Load} & & \text {Length} & & \text {Diameter} \\ \hline \boldsymbol{N} & \boldsymbol{l b}_{f} & \boldsymbol{m m} & \text { in. } & {\boldsymbol{m m}} & \text { in. } \\ \hline 46,100 & 10,400 & 56.896 & 2.240 & 11.71 & 0.461 \\ 44,800 & 10,100 & 57.658 & 2.270 & 11.26 & 0.443 \\ 42,600 & 9,600 & 58.420 & 2.300 & 10.62 & 0.418 \\ 36,400 & 8,200 & 59.182 & 2.330 & 9.40 & 0.370 \\ \hline \end{array} $$

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.

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