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A cylindrical fuel rod \(2 \mathrm{~cm}\) in diameter is encased in a concentric tube and cooled by water. The fuel generates heat uniformly at a rate of $150 \mathrm{MW} / \mathrm{m}^{3}$. The convection heat transfer coefficient on the fuel rod is \(5000 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\), and the average temperature of the cooling water, sufficiently far from the fuel rod, is \(70^{\circ} \mathrm{C}\). Determine the surface temperature of the fuel rod, and discuss whether the value of the given convection heat transfer coefficient on the fuel rod is reasonable.

Short Answer

Expert verified
Answer: Following the steps above, we calculate the surface temperature, \(T_s\), of the cylindrical fuel rod. We then compare this with the cooling water temperature, and if the difference is too large or unrealistic, the given convection heat transfer coefficient may not be reasonable. The reasonability of the convection heat transfer coefficient can also be assessed by comparing it with typical values found in literature or real-life scenarios.

Step by step solution

01

Find the heat generation rate per unit volume of the rod

The given heat generation rate is \(150 \mathrm{MW} / \mathrm{m}^{3}\) which needs to be converted to \(\mathrm{W} / \mathrm{m}^{3}\). $$ Q_{gen} = 150 \times 10^6 \mathrm{~W} / \mathrm{m}^{3} $$
02

Calculate the cross-sectional area of the cylindrical fuel rod

The diameter of the fuel rod is given as \(2 \mathrm{~cm}\). We need to convert it to meters and compute the cross-sectional area, \(A\), using the formula for the area of a circle: $$ A = \pi r^{2} = \pi (0.01 \mathrm{m})^{2} $$
03

Compute the heat generated per unit length of the fuel rod

Multiply the heat generation rate per unit volume, \(Q_{gen}\), with the cross-sectional area, \(A\), to find the heat generated per unit length, \(q'\): $$ q' = Q_{gen} \times A $$
04

Use the convection heat transfer equation to find the surface temperature

The convection heat transfer equation is given by: $$ q' = h A (T_{s} - T_{\infty}) $$ Where \(h\) is the convection heat transfer coefficient, \(A\) is the surface area of the fuel rod (per unit length), \(T_{s}\) is the surface temperature of the fuel rod, and \(T_{\infty}\) is the temperature of the cooling water far from the fuel rod. We are given \(h = 5000 \mathrm{~W} / \mathrm{m}^{2} \mathrm{K}\), and \(T_{\infty}= 70^{\circ} \mathrm{C}\). Substitute the given values and the values calculated in Steps 2 and 3: $$ q' = h (2 \pi r) (T_{s} - T_{\infty}) $$ Next, we need to isolate \(T_{s}\) in the above equation and then calculate the value for \(T_{s}\): $$ T_{s} = \frac{q'}{h (2 \pi r)} + T_{\infty} $$
05

Discuss the reasonability of the given convection heat transfer coefficient

Compare our calculated surface temperature with the cooling water temperature. If the difference between the surface temperature and the cooling water temperature is too large or unrealistic, then the given convection heat transfer coefficient may not be reasonable. Also, compare the convection heat transfer coefficient value with typical values found in literature or real-life scenarios.

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Most popular questions from this chapter

Which expression is used to determine the heat flux for conduction? (a) \(-k A \frac{d T}{d x}\) (b) \(-k \operatorname{grad} T\) (c) \(h\left(T_{2}-T_{1}\right)\) (d) \(\varepsilon \sigma T^{4}\) (e) None of them

An engineer who is working on the heat transfer analysis of a house in English units needs the convection heat transfer coefficient on the outer surface of the house. But the only value he can find from his handbooks is $14 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, which is in SI units. The engineer does not have a direct conversion factor between the two unit systems for the convection heat transfer coefficient. Using the conversion factors between \(\mathrm{W}\) and \(\mathrm{Btu} / \mathrm{h}, \mathrm{m}\) and \(\mathrm{ft}\), and \({ }^{\circ} \mathrm{C}\) and \({ }^{\circ} \mathrm{F}\), express the given convection heat transfer coefficient in Btu/h \(\mathrm{ft}^{2}{ }^{\circ} \mathrm{F}\). Answer: \(2.47\) Btu/h $\cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$

Consider a 20-cm-thick granite wall with a thermal conductivity of $2.79 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$. The temperature of the left surface is held constant at \(50^{\circ} \mathrm{C}\), whereas the right face is exposed to a flow of \(22^{\circ} \mathrm{C}\) air with a convection heat transfer coefficient of \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Neglecting heat transfer by radiation, find the right wall surface temperature and the heat flux through the wall.

Consider a person standing in a room at \(23^{\circ} \mathrm{C}\). Determine the total rate of heat transfer from this person if the exposed surface area and the skin temperature of the person are \(1.7 \mathrm{~m}^{2}\) and $32^{\circ} \mathrm{C}\(, respectively, and the convection heat transfer coefficient is \)5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Take the emissivity of the skin and the clothes to be \(0.9\), and assume the temperature of the inner surfaces of the room to be the same as the air temperature.

Consider a house in Atlanta, Georgia, that is maintained at $22^{\circ} \mathrm{C}\( and has a total of \)20 \mathrm{~m}^{2}$ of window area. The windows are double-door type with wood frames and metal spacers and have a \(U\)-factor of \(2.5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (see Prob. 1-120 for the definition of \(U\)-factor). The winter average temperature of Atlanta is \(11.3^{\circ} \mathrm{C}\). Determine the average rate of heat loss through the windows in winter.

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