Chapter 6: Problem 36
What is the physical significance of the Reynolds number? How is it defined for external flow over a plate of length \(L\) ?
Chapter 6: Problem 36
What is the physical significance of the Reynolds number? How is it defined for external flow over a plate of length \(L\) ?
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Get started for freeMost correlations for the convection heat transfer coefficient use the dimensionless Nusselt number, which is defined as (a) \(h / k\) (b) \(\mathrm{k} / \mathrm{h}\) (c) \(h L_{c} / k\) (d) \(k L_{c} / h\) (e) \(k / \rho c_{p}\)
Evaluate the Prandtl number from the following data: $c_{p}=0.5 \mathrm{Btu} / \mathrm{lbm} \cdot \mathrm{R}, k=2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot \mathrm{R}, \mu=0.3 \mathrm{lbm} / \mathrm{ft} \cdot \mathrm{s}$.
A cryogenic gas flows at \(5 \mathrm{~m} / \mathrm{s}\) in parallel over the plate. The temperature of the cold gas is \(-50^{\circ} \mathrm{C}\), and the plate length is \(1 \mathrm{~m}\). 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). In the interest of designing a heater, determine the total heat flux on the plate surface necessary to maintain the surface temperature at \(-30^{\circ} \mathrm{C}\). Use the following gas properties for the analysis: $c_{p}=1.002 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}, k=0.02057 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=1.527 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\(, and \)\rho=1.514 \mathrm{~kg} / \mathrm{m}^{3}$.
The upper surface of an ASTM B152 copper plate is subjected to convection with
hot air flowing at \(6 \mathrm{~m} / \mathrm{s}\) parallel over the plate
surface. The length of the plate is \(1 \mathrm{~m}\), and the temperature of
the hot air is \(400^{\circ} \mathrm{C}\). The maximum use temperature for the
ASTM B152 copper plate is \(260^{\circ} \mathrm{C}\) (ASME Code for Process
Piping, ASME B31.3-2014, Table A-1M). Determine the variation of the local
heat flux with the thermal boundary layer thickness on the plate surface for
\(0
Consider a laminar ideal gas flow over a flat plate, where the local Nusselt number can be expressed as $\mathrm{Nu}_{x}=0.332 \mathrm{Re}_{x}^{1 / 2} \operatorname{Pr}^{1 / 3}$. Using the expression for the local Nusselt number, show that it can be rewritten in terms of local convection heat transfer coefficient as \(h_{x}=C[V /(x T)]^{w}\), where \(C\) and \(m\) are constants.
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