Chapter 6: Problem 37
What is turbulent thermal conductivity? What is it caused by?
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Chapter 6: Problem 37
What is turbulent thermal conductivity? What is it caused by?
These are the key concepts you need to understand to accurately answer the question.
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For steady two-dimensional flow over an isothermal flat plate in the \(x\)-direction, express the boundary conditions for the velocity components \(u\) and \(v\), and the temperature \(T\) at the plate surface and at the edge of the boundary layer.
In turbulent flow, one can estimate the Nusselt number using the analogy between heat and momentum transfer (Colburn analogy). This analogy relates the Nusselt number to the coefficient of friction, \(C_{f}\), as (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \operatorname{Pr}^{1 / 3}\) (b) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \operatorname{Pr}^{2 / 3}\) (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \operatorname{Pr}^{1 / 3}\) (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} \operatorname{Pr}^{2 / 3}\)
Metal plates are being cooled with air blowing in parallel over each plate. The average friction coefficient over each plate is given as \(C_{f}=1.33\left(\operatorname{Re}_{L}{ }^{-0.5}\right.\) for \(\operatorname{Re}_{L}<5 \times 10^{5}\). Each metal plate length parallel to the air flow is \(1 \mathrm{~m}\). Determine the average convection heat transfer coefficient for the plate, if the air velocity is \(5 \mathrm{~m} / \mathrm{s}\). Evaluate the air properties at \(20^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).
Consider a flow over a surface with the velocity and temperature profiles given as $$ \begin{aligned} &u(y)=C_{1}\left(y+y^{2}-y^{3}\right) \\ &T(y)=C_{2}-e^{-2 C_{2} y} \end{aligned} $$ where the coefficients \(C_{1}\) and \(C_{2}\) are constants. Determine the expressions for the friction coefficient \(\left(C_{f}\right)\) and the convection heat transfer coefficient \((h)\).
How does turbulent flow differ from laminar flow? For which flow is the heat transfer coefficient higher?
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