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A brass wire of diameter \(d=2.42 \mathrm{mm}\) is stretched tightly between rigid supports so that the tensile force is \(T=98 \mathrm{N}\) (see figure). The coefficient of thermal expansion for the wire is \(19.5 \times 10^{-6 / 8} \mathrm{C}\) and the modulus of elasticity is \(E=110 \mathrm{GPa}\) (a) What is the maximum permissible temperature drop \(\Delta T\) if the allowable shear stress in the wire is 60 MPa? (b) At what temperature change does the wire go slack?

Short Answer

Expert verified
(a) Max temperature drop is 18.2°C, (b) Wire goes slack at 10°C temperature drop.

Step by step solution

01

Calculate Cross-sectional Area

The diameter of the wire is given as \(d = 2.42\, \mathrm{mm}\). First, convert this into meters: \(2.42\, \mathrm{mm} = 2.42 \times 10^{-3}\, \mathrm{m}\). The cross-sectional area \(A\) of the wire, assuming it's a circular cross-section, is given by:\[ A = \frac{\pi d^2}{4} \]Substitute the diameter:\[ A = \frac{\pi (2.42 \times 10^{-3})^2}{4} \approx 4.6 \times 10^{-6} \, \mathrm{m}^2 \]
02

Find the Tensile Stress in the Wire

The tensile stress \(\sigma\) in the wire is given by:\[ \sigma = \frac{T}{A} \]where \(T = 98 \, \mathrm{N}\) and \(A \approx 4.6 \times 10^{-6} \, \mathrm{m}^2\). Substituting these values gives:\[ \sigma = \frac{98}{4.6 \times 10^{-6}} \approx 21.3 \, \mathrm{MPa} \]
03

Max Allowable Stress Condition

The problem states the maximum allowable shear stress is \(60 \, \mathrm{MPa}\). The tensile stress of 21.3 MPa is well below 60 MPa. However, the problem asks about permissible changes based on temperature, not direct shear stress limits. This means effects caused by temperature have to be managed alongside allowed stress.
04

Calculate Temperature Drop for Max Stress

The amount of change in stress with temperature due to thermal expansion is given by:\[ \Delta \sigma = E \alpha \Delta T \] Rearranging for the temperature change when stress reaches the max:\[ \Delta T = \frac{\Delta \sigma}{E \alpha} \]Where \(\Delta \sigma = 60 - 21.3 = 38.7 \, \mathrm{MPa}\), \(E = 110 \, \mathrm{GPa} = 110 \times 10^3 \, \mathrm{MPa}\), and \(\alpha = 19.5 \times 10^{-6} \, \mathrm{C^{-1}}\):\[ \Delta T = \frac{38.7}{110 \times 10^3 \times 19.5 \times 10^{-6}} \approx 18.2 \, \mathrm{C} \]
05

Condition for Wire Going Slack

The wire goes slack when the thermal stress reversal equals the tensile stress, effectively reducing the applied tensile stress to zero. So:\[ \Delta \sigma = 21.3 \, \mathrm{MPa} \]Using the same formula:\[ \Delta T = \frac{21.3}{110 \times 10^3 \times 19.5 \times 10^{-6}} \approx 10 \, \mathrm{C} \]

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Key Concepts

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

Thermal Expansion
Thermal expansion is a fundamental concept in the mechanics of materials. It refers to the way materials change in size due to changes in temperature. Brass, like many materials, expands when heated and contracts when cooled. This property is described by the coefficient of thermal expansion, which for brass is given as \(19.5 \times 10^{-6}\, \text{K}^{-1}\). This means that for every degree Celsius change in temperature, a brass object will expand or contract by a factor of \(19.5 \times 10^{-6}\) of its original length.

In the context of the exercise, the brass wire is subjected to temperature changes that can alter its tensile stress. The relationship is given by \(\Delta \sigma = E \alpha \Delta T\), where \(\Delta \sigma\) is the change in stress, \(E\) is the modulus of elasticity, and \(\Delta T\) is the temperature change. This formula underscores how significant thermal expansion can be, affecting the overall mechanical performance of the material under different thermal conditions.
Modulus of Elasticity
The modulus of elasticity, also known as Young’s modulus, is a measure of a material's elasticity. It gives us an idea of how much a material will deform under a certain amount of stress. For brass, \(E = 110 \, \text{GPa}\). This is equivalent to \(110 \times 10^3 \, \text{MPa}\), indicating that brass is a relatively stiff material.

In the exercise, the modulus of elasticity plays a crucial role. It connects the change in tensile stress with the change in temperature through the formula \(\Delta \sigma = E \alpha \Delta T\). This relationship means that for a given change in temperature, the amount of stress change can be predicted if \(E\), the modulus of elasticity, is known. The stiffer the material (higher \(E\)), the more stress change is expected for the same temperature change.
Tensile Stress
Tensile stress refers to the amount of stretching force (tensile force) experienced by a material divided by its cross-sectional area. It is quantified in units such as pascals (Pa) or megapascals (MPa).

In this exercise, we calculated the tensile stress in the wire using the formula \(\sigma = \frac{T}{A}\), where \(T = 98 \, \text{N}\) is the tensile force, and \(A\) is the cross-sectional area of the wire (approximately \(4.6 \times 10^{-6} \, \text{m}^2\)). This calculation results in a tensile stress of approximately \(21.3 \, \text{MPa}\).

This stress level is well below the maximum allowable shear stress of \(60 \, \text{MPa}\) specified in the exercise. This means the wire can safely take this tensile load without yielding. However, changes in thermal conditions must also be considered, as they can lead to additional stress changes.
Cross-Sectional Area
The cross-sectional area of a wire is vital in determining the resistance to mechanical stresses. For cylindrical objects like wires, the cross-sectional area \(A\) is calculated using the formula: \(A = \frac{\pi d^2}{4}\), where \(d\) is the diameter of the wire.

In the case of the brass wire with a diameter of \(2.42\, \text{mm}\), it is first converted to meters: \(2.42 \times 10^{-3} \, \text{m}\). Substituting this diameter into the formula yields an area of approximately \(4.6 \times 10^{-6}\, \text{m}^2\).

This calculated cross-sectional area is essential for further calculations of tensile stress. It allows for the determination of how much force the wire can withstand per unit area. A larger cross-sectional area means that the wire can shoulder more force without reaching its tensile strength limit.

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Most popular questions from this chapter

A plastic bar of rectangular cross section \((b=38 \mathrm{mm}\) and \(h=75 \mathrm{mm}\) ) fits snugly between rigid supports at room temperature \(\left(20^{\circ} \mathrm{C}\right)\) but with no initial stress (see figure). When the temperature of the bar is raised to \(70^{\circ} \mathrm{C}\), the compressive stress on an inclined plane \(p q\) at midspan becomes \(8.7 \mathrm{MPa}\) (a) What is the shear stress on plane \(p q ?\) (Assume \(\alpha=95 \times 10^{-6 /^{\circ}} \mathrm{C} \text { and } E=2.4 \mathrm{GPa}\) (b) Draw a stress element oriented to plane \(p q\) and show the stresses acting on all faces of this element. (c) If the allowable normal stress is 23 MPa and the allowable shear stress is \(11.3 \mathrm{MPa}\), what is the maximum load \(P(\text {in }+x \text { direction })\) which can be added at the quarter point (in addition to thermal effects given) without exceeding allowable stress values in the bar?

Two identical bars \(A B\) and \(B C\) support a vertical load \(P\) (see figure). The bars are made of steel having a stress-strain curve that may be idealized as elastoplastic with yield stress \(\sigma_{Y}\) Each bar has cross-sectional area \(A\) Determine the yield load \(P_{Y}\) and the plastic load \(P_{P^{-}}\)

A plastic rod \(A B\) of length \(L=0.5 \mathrm{m}\) has a diameter \(d_{1}=30 \mathrm{mm}\) (see figure). A plastic sleeve \(C D\) of length \(c=0.3 \mathrm{m}\) and outer diameter \(d_{2}=45 \mathrm{mm}\) is securely bonded to the rod so that no slippage can occur between the rod and the sleeve. The rod is made of an acrylic with modulus of elasticity \(E_{1}=3.1 \mathrm{GPa}\) and the sleeve is made of a polyamide with \(E_{2}=2.5 \mathrm{GPa}\) (a) Calculate the elongation \(\delta\) of the rod when it is pulled by axial forces \(P=12 \mathrm{kN}\) (b) If the sleeve is extended for the full length of the rod, what is the clongation? (c) If the sleeve is removed, what is the elongation?

A flat bar of rectangular cross section, length \(L\) and constant thickness \(t\) is subjected to tension by forces \(P\) (see figure). The width of the bar varies linearly from \(b_{1}\) at the smaller end to \(b_{2}\) at the larger end. Assume that the angle of taper is small. (a) Derive the following formula for the elongation of the bar: $$\delta=\frac{P L}{E t\left(b_{2}-b_{1}\right)} \ln \frac{b_{2}}{b_{1}}$$ (b) Calculate the elongation, assuming \(L=1.5 \mathrm{m}\)\\[\begin{array}{l}t=25 \mathrm{mm}, P=125 \mathrm{kN},b_{1}=100 \mathrm{mm}, b_{2}=150 \mathrm{mm}, \text { and } \\\E=200 \mathrm{GPa}\end{array}\\]

A hollow circular tube \(T\) of length \(L=380 \mathrm{mm}\) is uniformly compressed by a force \(P\) acting through a rigid plate (see figure). The outside and inside diameters of the tube are 76 and \(70 \mathrm{mm}\), respectively. A concentric solid circular bar \(B\) of \(38 \mathrm{mm}\) diameter is mounted inside the tube. When no load is present, there is a clearance \(c=\) \(0.26 \mathrm{mm}\) between the bar \(B\) and the rigid plate. Both bar and tube are made of steel having an elastoplastic stress-strain diagram with \(E=200 \mathrm{GPa}\) and \(\sigma_{Y}=250 \mathrm{MPa}\) (a) Determine the yield load \(P_{Y}\) and the corresponding shortening \(\delta_{Y}\) of the tube. (b) Determine the plastic load \(P_{P}\) and the corresponding shortening \(\delta_{P}\) of the tube. (c) Construct a load-displacement diagram showing the load \(P\) as ordinate and the shortening \(\delta\) of the tube as abscissa. (Hint: The load-displacement diagram is not a single straight line in the region \(0 \leq P \leq P_{Y}\).)

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