Chapter 6: Problem 6
What is the physical significance of the Nusselt number? How is it defined?
Chapter 6: Problem 6
What is the physical significance of the Nusselt number? How is it defined?
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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) \(k / \rho c_{p}\)
Consider fluid flow over a surface with a velocity profile given as $$ u(y)=100\left(y+2 y^{2}-0.5 y^{3}\right) \mathrm{m} / \mathrm{s} $$ Determine the shear stress at the wall surface, if the fluid is (a) air at $1 \mathrm{~atm}\( and (b) liquid water, both at \)20^{\circ} \mathrm{C}$. Also calculate the wall shear stress ratio for the two fluids, and interpret the result.
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 $1 \mathrm{~atm}$.
The transition from laminar flow to turbulent flow in a forced convection situation is determined by which one of the following dimensionless numbers? (a) Grasshof (b) Nusselt (c) Reynolds (d) Stanton (e) Mach
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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