Chapter 6: Problem 36
What is turbulent viscosity? What is it caused by?
Chapter 6: Problem 36
What is turbulent viscosity? What is it caused by?
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Get started for freeWhen is heat transfer through a fluid conduction and when is it convection? For what case is the rate of heat transfer higher? How does the convection heat transfer coefficient differ from the thermal conductivity of a fluid?
An airfoil with a characteristic length of \(0.2 \mathrm{ft}\) is placed in airflow at \(1 \mathrm{~atm}\) and \(60^{\circ} \mathrm{F}\) with free stream velocity of \(150 \mathrm{ft} / \mathrm{s}\) and convection heat transfer coefficient of \(21 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\). If a second airfoil with a characteristic length of \(0.4 \mathrm{ft}\) is placed in the airflow at \(1 \mathrm{~atm}\) and \(60^{\circ} \mathrm{F}\) with free stream velocity of \(75 \mathrm{ft} / \mathrm{s}\), determine the heat flux from the second airfoil. Both airfoils are maintained at a constant surface temperature of \(180^{\circ} \mathrm{F}\).
A 6-cm-diameter shaft rotates at \(3000 \mathrm{rpm}\) in a 20 -cm-long bearing with a uniform clearance of \(0.2 \mathrm{~mm}\). At steady operating conditions, both the bearing and the shaft in the vicinity of the oil gap are at \(50^{\circ} \mathrm{C}\), and the viscosity and thermal conductivity of lubricating oil are \(0.05 \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\) and \(0.17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). By simplifying and solving the continuity, momentum, and energy equations, determine \((a)\) the maximum temperature of oil, \((b)\) the rates of heat transfer to the bearing and the shaft, and \((c)\) the mechanical power wasted by the viscous dissipation in the oil.
What is external forced convection? How does it differ from internal forced convection? Can a heat transfer system involve both internal and external convection at the same time? Give an example.
Air flowing over a \(1-\mathrm{m}\)-long flat plate at a velocity of \(7 \mathrm{~m} / \mathrm{s}\) has a friction coefficient given as \(C_{f}=0.664(V x / \nu)^{-0.5}\), where \(x\) is the location along the plate. Determine the wall shear stress and the air velocity gradient on the plate surface at mid-length of the plate. Evaluate the air properties at \(20^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).
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