Chapter 6: Problem 33
What fluid property is responsible for the development of the velocity boundary layer? For what kinds of fluids will there be no velocity boundary layer on a flat plate?
Chapter 6: Problem 33
What fluid property is responsible for the development of the velocity boundary layer? For what kinds of fluids will there be no velocity boundary layer on a flat plate?
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Get started for freeObject 1 with a characteristic length of \(0.5 \mathrm{~m}\) is placed in airflow at \(1 \mathrm{~atm}\) and \(20^{\circ} \mathrm{C}\) with free stream velocity of \(50 \mathrm{~m} / \mathrm{s}\). The heat flux transfer from object 1 when placed in the airflow is measured to be $12,000 \mathrm{~W} / \mathrm{m}^{2}$. If object 2 has the same shape and geometry as object 1 (but with a characteristic length of \(5 \mathrm{~m}\) ) and it is placed in the airflow at \(1 \mathrm{~atm}\) and \(20^{\circ} \mathrm{C}\) with free stream velocity of \(5 \mathrm{~m} / \mathrm{s}\), determine the average convection heat transfer coefficient for object 2 . Both objects are maintained at a constant surface temperature of \(120^{\circ} \mathrm{C}\).
Consider steady, laminar, two-dimensional flow over an isothermal plate. Does the wall shear stress increase, decrease, or remain constant with distance from the leading edge?
In which mode of heat transfer is the convection heat transfer coefficient usually higher, natural convection or forced convection? Why?
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, \(C_{p}\) as (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (e) \(\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3}\) (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} P r^{2 / 3}\)
What is the physical significance of the Nusselt number? How is it defined?
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