A cylindrical specimen of a titanium alloy having an elastic modulus of \(107 \mathrm{GPa}\) (15.5 \(\times\) \(10^{6} \mathrm{psi}\) ) and an original diameter of \(3.8 \mathrm{~mm}\) (0.15 in.) will experience only elastic deformation when a tensile load of \(2000 \mathrm{~N}\) \(\left(450 \mathrm{lb}_{\mathrm{f}}\right)\) is applied. Compute the maximum length of the specimen before deformation if the maximum allowable elongation is \(0.42\) \(\mathrm{mm}(0.0165\) in.).

Short Answer

Expert verified
Answer: The maximum length of the specimen before deformation is approximately 255.16 mm.

Step by step solution

01

Compute the stress

We can compute the stress experienced by the specimen using the given force and cross-sectional area. We will first calculate the cross-sectional area of the cylindrical specimen and then find the stress. The cross-sectional area \(A\) of the cylinder is given by the equation: \(A = \pi (\frac{d}{2})^2\) where \(d\) is the diameter of the cylinder. Given that the diameter of the specimen is \(d=3.8 \mathrm{~mm}\), the cross-sectional area of the specimen is: \(A = \pi (\frac{3.8}{2})^2 = 11.35 \mathrm{~mm^2}\) Now that we have the area, we can calculate the stress \(\sigma\) by dividing the tensile load \(F\) by the area \(A\): \(\sigma = \frac{F}{A}\) Given the tensile load of \(F=2000 \mathrm{~N}\): \(\sigma = \frac{2000}{11.35} = 176.20 \mathrm{~MPa}\)
02

Compute the strain

Now that we have the stress, we can use Hooke's law to calculate the strain \(\epsilon\). Hooke's Law states that stress is proportional to strain: \(\sigma = E \epsilon\) where \(E\) is the elastic modulus, and \(\epsilon\) is the strain. Given the elastic modulus of \(E = 107 \mathrm{GPa}\) or \(107000 \mathrm{MPa}\), we can rearrange the equation and find the strain: \(\epsilon = \frac{\sigma}{E} = \frac{176.20}{107000} = 1.646 \times 10^{-3}\)
03

Calculate the original length

Now, we can use the relationship between the strain, elongation, and original length to find the original length of the specimen. The strain is equal to the elongation divided by the original length: \(\epsilon = \frac{\Delta L}{L}\) where \(\Delta L\) is the elongation and \(L\) is the original length. We are given the maximum allowable elongation as \(\Delta L = 0.42 \mathrm{mm}\). Rearranging the equation to solve for \(L\): \(L = \frac{\Delta L}{\epsilon}\) Substituting the values, we get: \(L = \frac{0.42}{1.646 \times 10^{-3}} = 255.16 \mathrm{mm}\) So, the maximum length of the specimen before deformation is approximately \(255.16 \mathrm{mm}\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Elastic Modulus
When we talk about the elastic modulus of a material, we are referring to a measurement of its ability to withstand changes in length when under tension or compression. It is a fundamental property that quantifies the stiffness of a solid material. In the context of the exercise, the elastic modulus represents how much a titanium alloy can deform elastically—the range in which the material will return to its original shape once the load is removed.

To understand this with a real-world analogy, think of the elastic modulus as a measure of how 'springy' a material is. Just as a spring can stretch and then return to its original position, materials with a high elastic modulus will undergo less deformation under a tensile load before returning to their initial state.

For calculations, the elastic modulus (E) is typically expressed in units of pressure, such as pascals (Pa) or gigapascals (GPa). In the exercise, the elastic modulus of the titanium alloy is given as 107 GPa, which means it is relatively stiff and resistant to deformation under the applied loads.
Tensile Load
The concept of a tensile load refers to a force that attempts to stretch a material by pulling it apart. This is the kind of force that the cylindrical titanium alloy specimen experiences in the exercise. It is an important aspect of mechanical engineering and material science, as understanding how materials respond to tensile forces is crucial for design and safety.

To better understand tensile force, picture a rope in a tug-of-war game. The pulling force each team applies to the rope is akin to the tensile load. In the exercise, the cylindrical specimen is subjected to a tensile load of 2000 N. The impact of this force depends not only on its magnitude but also on the area over which it is applied, which is why calculating the cross-sectional area is a necessary step to evaluate the resulting stress on the material.
Strain Calculation
Strain is a measure of how much a material deforms relative to its original length when a force is applied. Strain calculation is critical in engineering because it helps predict how a structure will behave under various loads, ensuring that designs are safe and effective.

The strain is expressed as a dimensionless ratio, calculated by dividing the change in length (ΔL), also known as elongation, by the original length (L) of the material. Mathematically, it's represented as \(\epsilon = \frac{\Delta L}{L}\).

In the step-by-step solution presented, we use given values to compute the strain experienced by the titanium alloy when subjected to a specified tensile load. This value helps us understand how much the material will stretch without causing permanent deformation, ensuring that the structural integrity of the material is not compromised when in use.

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Most popular questions from this chapter

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.

A specimen of aluminum having a rectangular cross section \(10 \mathrm{~mm} \times 12.7 \mathrm{~mm}(0.4\) in. \(\times 0.5\) in.) is pulled in tension with \(35,500 \mathrm{~N}\) \(\left(8000 \mathrm{lb}_{\mathrm{f}}\right)\) force, producing only elastic deformation. Calculate the resulting strain.

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 cylindrical specimen of an alloy \(8 \mathrm{~mm}\) (0.31 in.) in diameter is stressed elastically in tension. A force of \(15,700 \mathrm{~N}\) (3530 lb_{f } \()\) produces a reduction in specimen diameter of \(5 \times 10^{-3} \mathrm{~mm}\left(2 \times 10^{-4}\right.\) in.). Compute Poisson's ratio for this material if its modulus of elasticity is \(140 \mathrm{GPa}\left(20.3 \times 10^{6} \mathrm{psi}\right)\).

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 \(0.25\) ?

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