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In cryogenic equipment, cold gas flows in parallel over the surface of a \(1-\mathrm{m}\)-long plate. The gas velocity is \(4 \mathrm{~m} / \mathrm{s}\) at a temperature of \(-70^{\circ} \mathrm{C}\). The gas has a thermal conductivity of \(0.01979 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), a kinematic viscosity of \(9.319 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\), and a Prandtl number of \(0.7440\). A stainless steel (ASTM A437 B4B) bolt is embedded in the plate at midlength. 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). To keep the bolt from getting below its minimum suitable temperature, the plate is subjected to a uniform heat flux of $250 \mathrm{~W} / \mathrm{m}^{2}$. Determine whether the heat flux to the plate is sufficient to keep the bolt above the minimum suitable temperature of \(-30^{\circ} \mathrm{C}\).

Short Answer

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Re ≈ 4293.౩

Step by step solution

01

Calculate the Reynolds number

The Reynolds number is needed to determine the flow regime and heat transfer characteristics. It can be determined by the formula: Re = (U*L)/ν where Re is the Reynolds number, U is the gas velocity, L is the length of the plate, and ν is the kinematic viscosity. Re = (4 * 1)/(9.319 * 10^{-6}) Calculate Re:

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Most popular questions from this chapter

Air at \(25^{\circ} \mathrm{C}\) flows over a 5 -cm-diameter, \(1.7-\mathrm{m}\)-long smooth pipe with a velocity of $4 \mathrm{~m} / \mathrm{s}\(. A refrigerant at \)-15^{\circ} \mathrm{C}$ flows inside the pipe, and the surface temperature of the pipe is essentially the same as the refrigerant temperature inside. The drag force exerted on the pipe by the air is (a) \(0.4 \mathrm{~N}\) (b) \(1.1 \mathrm{~N}\) (c) \(8.5 \mathrm{~N}\) (d) \(13 \mathrm{~N}\) (e) \(18 \mathrm{~N}\) (For air, use $\nu=1.382 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, \rho=1.269 \mathrm{~kg} / \mathrm{m}^{3}$ )

A cylindrical rod is placed in a crossflow of air at $20^{\circ} \mathrm{C}(1 \mathrm{~atm})\( with velocity of \)10 \mathrm{~m} / \mathrm{s}$. The rod has a diameter of \(5 \mathrm{~mm}\) and a constant surface temperature of \(120^{\circ} \mathrm{C}\). Determine \((a)\) the average drag coefficient, \((b)\) the convection heat transfer coefficient using the Churchill and Bernstein relation, and (c) the convection heat transfer coefficient using Table 7-1.

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Hydrogen gas at \(1 \mathrm{~atm}\) is flowing in parallel over the upper and lower surfaces of a 3 -m-long flat plate at a velocity of $2.5 \mathrm{~m} / \mathrm{s}\(. The gas temperature is \)120^{\circ} \mathrm{C}$, and the surface temperature of the plate is maintained at \(30^{\circ} \mathrm{C}\). Using appropriate software, investigate the local convection heat transfer coefficient and the local total convection heat flux along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient and the local total convection heat flux as functions of \(x\). Assume flow is laminar, but make sure to verify this assumption.

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