Chapter 7: Problem 12
Consider laminar flow over a flat plate. Will the friction coefficient change with distance from the leading edge? How about the heat transfer coefficient?
Chapter 7: Problem 12
Consider laminar flow over a flat plate. Will the friction coefficient change with distance from the leading edge? How about the heat transfer coefficient?
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Get started for freeA \(15-\mathrm{cm} \times 15-\mathrm{cm}\) circuit board dissipating $20 \mathrm{~W}$ of power uniformly is cooled by air, which approaches the circuit board at \(20^{\circ} \mathrm{C}\) with a velocity of $6 \mathrm{~m} / \mathrm{s}$. Disregarding any heat transfer from the back surface of the board, determine the surface temperature of the electronic components \((a)\) at the leading edge and \((b)\) at the end of the board. Assume the flow to be turbulent since the electronic components are expected to act as turbulators. For air properties evaluations, assume a film temperature of $35^{\circ} \mathrm{C}$. Is this a good assumption?
In cryogenic equipment, cold air flows in parallel over the surface of a \(2-\mathrm{m} \times 2-\mathrm{m}\) ASTM A240 \(410 \mathrm{~S}\) stainless steel plate. The air velocity is \(5 \mathrm{~m} / \mathrm{s}\) at a temperature of \(-70^{\circ} \mathrm{C}\). The minimum temperature suitable for the ASTM A240 \(410 \mathrm{~S}\) plate is \(-30^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-1M). The plate is heated to keep its surface temperature from going below \(-30^{\circ} \mathrm{C}\). Determine the average heat transfer rate required to keep the plate surface from getting below the minimum suitable temperature.
Define the frontal area of a body subjected to external flow. When is it appropriate to use the frontal area in drag and lift calculations?
stream is to be measured by a thermocouple with a spherical junction. Due to the nature of this experiment, the response time of the thermocouple to register 99 percent of the initial temperature difference must be within $5 \mathrm{~s}\(. The properties of the thermocouple junction are \)k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\rho=8500 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)c_{p}=320 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}$. The hot air has a freestream velocity and temperature of $3 \mathrm{~m} / \mathrm{s}\( and \)140^{\circ} \mathrm{C}$, respectively. If the initial temperature of the thermocouple junction is \(20^{\circ} \mathrm{C}\), determine the thermocouple junction diameter that would satisfy the required response time of \(5 \mathrm{~s}\). Hint: Use lumped system analysis to determine the time required for the thermocouple to register 99 percent of the initial temperature difference (verify the application of this method to this problem).
Steam at \(250^{\circ} \mathrm{C}\) flows in a stainless steel pipe $(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ whose inner and outer diameters are \(4 \mathrm{~cm}\) and \(4.6 \mathrm{~cm}\), respectively. The pipe is covered with \(3.5-\mathrm{cm}\)-thick glass wool insulation $(k=0.038 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( whose outer surface has an emissivity of \)0.3$. Heat is lost to the surrounding air and surfaces at \(3^{\circ} \mathrm{C}\) by convection and radiation. Taking the heat transfer coefficient inside the pipe to be \(80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the rate of heat loss from the steam per unit length of the pipe when air is flowing across the pipe at \(4 \mathrm{~m} / \mathrm{s}\). Evaluate the air properties at a film temperature of \(10^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).
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