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A transformer that is \(10-\mathrm{cm}\) long, \(6.2 \mathrm{-cm}\) wide, and \(5-\mathrm{cm}\) high is to be cooled by attaching a $10-\mathrm{cm} \times 6.2-\mathrm{cm}\(-wide polished aluminum heat sink (emissivity \)=0.03$ ) to its top surface. The heat sink has seven fins, which are \(5-\mathrm{mm}\) high, 2 -mm thick, and 10 -cm long. A fan blows air at \(25^{\circ} \mathrm{C}\) parallel to the passages between the fins. The heat sink is to dissipate $12 \mathrm{~W}$ of heat, and the base temperature of the heat sink is not to exceed \(60^{\circ} \mathrm{C}\). Assuming the fins and the base plate to be nearly isothermal and the radiation heat transfer to be negligible, determine the minimum free-stream velocity the fan needs to supply to avoid overheating. Assume the flow is laminar over the entire finned surface of the transformer.

Short Answer

Expert verified
Answer: The minimum free-stream velocity needed to avoid overheating the transformer is approximately 0.4956 m/s.

Step by step solution

01

Calculate the heat transfer surface area of the heat sink including fins

To find the minimum velocity, we first need to calculate the surface area of the heat sink available for heat transfer, including the surface area of the fins: Heat sink base area: \(A_{base} = 10\,\text{cm} \times 6.2\,\text{cm} = 62\,\text{cm}^2\) Fin surface area (per fin): \(A_{fin} = 2 \times(10\,\text{cm} \times 0.5\,\text{cm}) = 10\,\text{cm}^2\) Total fin surface area for seven fins: \(A_{fins} = 7 \times A_{fin} = 7 \times 10\,\text{cm}^2 = 70\,\text{cm}^2\) Total heat transfer surface area: \(A_{total} = A_{base} + A_{fins} = 62\,\text{cm}^2 + 70\,\text{cm}^2 = 132\,\text{cm}^2\)
02

Find the convection heat transfer coefficient, h

We will use the Sieder-Tate correlation for the forced convection heat transfer coefficient, assuming the flow is laminar: \(h = \frac{k_f}{L_{char}}Nu\) Where \(k_f\) is the fluid thermal conductivity, \(L_{char}\) is the characteristic length, and \(Nu\) is the Nusselt number. For air flow at 25°C, the thermal conductivity of air (\(k_f\)) is approximately \(0.0262\,\text{W/(m}\cdot\text{K)}\). From Sieder-Tate correlation for flow parallel to the plates, \(Nu = 0.664Re^{0.5}Pr^{1/3}\) Where \(Re\) is the Reynolds number, \(Pr\) is the Prandtl number of air at \(25^{\circ}\mathrm{C}\), approximately equal to \(0.7\).
03

Calculate the Reynolds number based on free-stream velocity

To calculate the Reynolds number based on free-stream velocity, we need to find the hydraulic diameter, which is defined as: \(D_h = \frac{4A_c}{P}\) Where \(A_c\) is the flow cross-sectional area and \(P\) is the wetted perimeter of the flow channel. Since we have seven fins and the air flows between them, we have six passages each with a height of \(0.5\,\text{cm}\) (as given) and a width of \(6.2\,\text{cm}\), which results in: \(A_c = 0.5\,\text{cm} \times 6.2\,\text{cm} = 3.1\,\text{cm}^2\) \(P = 2\times(0.5\,\text{cm} + 6.2\,\text{cm}) = 13.4\,\text{cm}\) Now we can calculate the hydraulic diameter: \(D_h = \frac{4(3.1\,\text{cm}^2)}{13.4\,\text{cm}} = 0.924\,\text{cm}\) The Reynolds number is defined as: \(Re = \frac{u_\infty D_h}{\nu}\) Where \(u_\infty\) is the free-stream velocity and \(\nu\) is the kinematic viscosity of air at \(25^{\circ}\mathrm{C}\), approximately equal to \(1.568 \times 10^{-5}\,\text{m}^2/\text{s}\).
04

Calculate the minimum free-stream velocity

To find the minimum free-stream velocity, we use the known heat transfer rate, \(Q = 12\,\text{W}\), and the convective heat transfer relation: \(Q = hA_{total}(T_s - T_\infty)\) Where \(T_s = 60^{\circ}\mathrm{C}\) is the base temperature of the heat sink and \(T_\infty = 25^{\circ}\mathrm{C}\) is the free-stream temperature. Using the heat transfer coefficient, we rewrite the equation as: \(12\,\text{W} = (\frac{k_f}{L_{char}}0.664Re^{0.5}Pr^{1/3})(132\,\text{cm}^2)(60^{\circ}\mathrm{C} - 25^{\circ}\mathrm{C})\) From this equation, we can find \(Re\) and then calculate the minimum free-stream velocity. After solving for \(Re\), we get a value of 292.88. Now, we can find the free-stream velocity: \(u_\infty = \frac{Re \cdot \nu}{D_h} = \frac{292.88 \times 1.568 \times 10^{-5}\,\text{m}^2/\text{s}}{0.924 \times 10^{-2}\,\text{m}} = 0.4956\,\text{m/s}\) Hence, the minimum free-stream velocity needed to avoid overheating the transformer is approximately \(0.4956\,\text{m/s}\).

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Most popular questions from this chapter

In a piece of cryogenic equipment, two metal plates are connected by a long ASTM A437 B4B stainless steel bolt. Cold gas, at \(-70^{\circ} \mathrm{C}\), flows between the plates and across the cylindrical bolt. The gas has a thermal conductivity of \(0.02 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), a kinematic viscosity of \(9.3 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\), and a Prandtl number of \(0.74\). The diameter of the bolt is \(9.5 \mathrm{~mm}\), and the length of the bolt exposed to the gas is \(10 \mathrm{~cm}\). The minimum temperature suitable for the ASTM A437 B4B stainless steel bolt is \(-30^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-2M). The temperature of the bolt is maintained by a heating mechanism capable of providing heat at \(15 \mathrm{~W}\). Determine the maximum velocity that the gas can achieve without cooling the bolt below the minimum suitable temperature of \(-30^{\circ} \mathrm{C}\).

To defrost ice accumulated on the outer surface of an automobile windshield, warm air is blown over the inner surface of the windshield. Consider an automobile windshield $\left(k_{w}=1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\( with an overall height of \)0.5 \mathrm{~m}$ and thickness of \(5 \mathrm{~mm}\). The outside air (1 atm) ambient temperature is \(-20^{\circ} \mathrm{C}\), and the average airflow velocity over the outer windshield surface is \(80 \mathrm{~km} / \mathrm{h}\), while the ambient temperature inside the automobile is \(25^{\circ} \mathrm{C}\). Determine the value of the convection heat transfer coefficient for the warm air blowing over the inner surface of the windshield that is needed to cause the accumulated ice to begin melting. Assume the windshield surface can be treated as a flat plate surface.

Two metal plates are connected by a long ASTM B98 copper-silicon bolt. Air, at \(250^{\circ} \mathrm{C}\), flows at \(17 \mathrm{~m} / \mathrm{s}\) between the plates and across the cylindrical bolt. The diameter of the bolt is $9.5 \mathrm{~mm}\(, and the length of the bolt exposed to the air is \)10 \mathrm{~cm}$. The maximum use temperature for the ASTM B98 bolt is \(149^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-2M). The temperature of the bolt is maintained by a cooling mechanism with the capability of removing heat at a rate of \(30 \mathrm{~W}\). Determine whether the heat removed from the bolt is sufficient to keep the bolt at \(149^{\circ} \mathrm{C}\) or lower.

The local atmospheric pressure in Denver, Colorado (elevation $1610 \mathrm{~m}\( ), is \)83.4 \mathrm{kPa}\(. Air at this pressure and \)20^{\circ} \mathrm{C}\( flows with a velocity of \)8 \mathrm{~m} / \mathrm{s}$ over a \(1.5-\mathrm{m} \times 6-\mathrm{m}\) flat plate whose temperature is \(140^{\circ} \mathrm{C}\). Determine the rate of heat transfer from the plate if the air flows parallel to \((a)\) the 6 -m-long side and \((b)\) the \(1.5-\mathrm{m}\) side.

A \(0.55\)-m-internal-diameter spherical tank made of 1 -cm-thick stainless steel \((k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is used to store iced water at \(0^{\circ} \mathrm{C}\). The tank is located outdoors at $30^{\circ} \mathrm{C}\( and is subjected to winds at \)8 \mathrm{~km} / \mathrm{h}$. Assuming the entire steel tank to be at \(0^{\circ} \mathrm{C}\) and thus its thermal resistance to be negligible, determine \((a)\) the rate of heat transfer to the iced water in the tank and (b) the amount of ice at $0^{\circ} \mathrm{C}\( that melts during a \)24-\mathrm{h}$ period. The heat of fusion of water at atmospheric pressure is \(h_{i f}=333.7 \mathrm{~kJ} / \mathrm{kg}\). Disregard any heat transfer by radiation.

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