Chapter 6: Problem 1
Define incompressible flow and incompressible fluid. Must the flow of a compressible fluid necessarily be treated as compressible?
Chapter 6: Problem 1
Define incompressible flow and incompressible fluid. Must the flow of a compressible fluid necessarily be treated as compressible?
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The upper surface of an ASME SB-96 coppersilicon plate is subjected to convection with hot air flowing at \(6.5 \mathrm{~m} / \mathrm{s}\) parallel over the plate surface. The plate is square with a length of \(1 \mathrm{~m}\), and the temperature of the hot air is \(200^{\circ} \mathrm{C}\). The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits equipment constructed with ASME SB-96 plate to be operated at a temperature not exceeding \(93^{\circ} \mathrm{C}\). From a wind tunnel experiment, the average friction coefficient for the upper surface of the plate was found to be \(0.0023\). In the interest of designing a cooling mechanism to keep the plate surface temperature from exceeding \(93^{\circ} \mathrm{C}\), determine the minimum heat removal rate required to keep the plate surface from going above \(93^{\circ} \mathrm{C}\). Use the following air properties for the analysis: $c_{p}=1.016 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}, k=0.03419 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\mu=2.371 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\(, and \)\rho=0.8412 \mathrm{~kg} / \mathrm{m}^{3}$.
Air flows over a flat plate at $40 \mathrm{~m} / \mathrm{s}, 25^{\circ} \mathrm{C}\(, and \)1 \mathrm{~atm}\( pressure. \)(a)$ What plate length should be used to achieve a Reynolds number of \(1 \times 10^{8}\) at the end of the plate? (b) If the critical Reynolds number is \(5 \times 10^{5}\), at what distance from the leading edge of the plate would transition occur?
In an effort to prevent the formation of ice on the surface of a wing, electrical heaters are embedded inside the wing. With a characteristic length of \(2.5 \mathrm{~m}\), the wing has a friction coefficient of \(0.001\). If the wing is moving at a speed of \(200 \mathrm{~m} / \mathrm{s}\) through air at $1 \mathrm{~atm}\( and \)-20^{\circ} \mathrm{C}$, determine the heat flux necessary to keep the wing surface above \(0^{\circ} \mathrm{C}\). Evaluate the air properties at \(-10^{\circ} \mathrm{C}\) and 1 atm.
Two metal plates are connected by a long ASTM B 98 copper-silicon bolt. A hot gas at \(200^{\circ} \mathrm{C}\) flows 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 hot gas is \(10 \mathrm{~cm}\). The average convection heat transfer coefficient for the bolt in crossflow is correlated with the gas velocity as \(h=24.6 \mathrm{~V}^{0.62}\), where \(h\) and \(V\) have the units \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and $\mathrm{m} / \mathrm{s}$, respectively. 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). If the gas velocity is \(10.4 \mathrm{~m} / \mathrm{s}\), determine the minimum heat removal rate required to keep the bolt surface from going above the maximum use temperature.
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