Chapter 7: Problem 67
In flow over cylinders, why does the drag coefficient suddenly drop when the flow becomes turbulent? Isn't turbulence supposed to increase the drag coefficient instead of decreasing it?
Chapter 7: Problem 67
In flow over cylinders, why does the drag coefficient suddenly drop when the flow becomes turbulent? Isn't turbulence supposed to increase the drag coefficient instead of decreasing it?
All the tools & learning materials you need for study success - in one app.
Get started for freeAir at \(15^{\circ} \mathrm{C}\) flows over a flat plate subjected to a uniform heat flux of \(240 \mathrm{~W} / \mathrm{m}^{2}\) with a velocity of $3.5 \mathrm{~m} / \mathrm{s}\(. The surface temperature of the plate \)6 \mathrm{~m}$ from the leading edge is (a) \(40.5^{\circ} \mathrm{C}\) (b) \(41.5^{\circ} \mathrm{C}\) (c) \(58.2^{\circ} \mathrm{C}\) (d) \(95.4^{\circ} \mathrm{C}\) (e) \(134^{\circ} \mathrm{C}\) (For air, use $k=0.02551 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7296, \nu=1.562 \times\( \)10^{-5} \mathrm{~m}^{2} / \mathrm{s}$ )
What is the effect of surface roughness on the friction drag coefficient in laminar and turbulent flows?
Jakob (1949) suggests the following correlation be used for square tubes in a liquid crossflow situation: $$ \mathrm{Nu}=0.102 \mathrm{Re}^{0.625} \mathrm{Pr}^{1 / 3} $$ Water \((k=0.61 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mathrm{Pr}=6)\) flows across a \(1-\mathrm{cm}-\) square tube with a Reynolds number of 10,000 . The convection heat transfer coefficient is (a) \(5.7 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) (b) \(8.3 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) (c) \(11.2 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) (d) \(15.6 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) (e) \(18.1 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\)
Air at \(20^{\circ} \mathrm{C}\) flows over a 4-m-long and 3-m-wide surface of a plate whose temperature is \(80^{\circ} \mathrm{C}\) with a velocity of $5 \mathrm{~m} / \mathrm{s}$. The rate of heat transfer from the laminar flow region of the surface is (a) \(950 \mathrm{~W}\) (b) \(1037 \mathrm{~W}\) (c) \(2074 \mathrm{~W}\) (d) \(2640 \mathrm{~W}\) (e) \(3075 \mathrm{~W}\) (For air, use $k=0.02735 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7228, \nu=1.798 \times\( \)10^{-5} \mathrm{~m}^{2} / \mathrm{s}$ )
A cylindrical rod is placed in a crossflow of air at $20^{\circ} \mathrm{C}(1 \mathrm{~atm})\( with velocity of \)10 \mathrm{~m} / \mathrm{s}$. The rod has a diameter of \(5 \mathrm{~mm}\) and a constant surface temperature of \(120^{\circ} \mathrm{C}\). Determine \((a)\) the average drag coefficient, \((b)\) the convection heat transfer coefficient using the Churchill and Bernstein relation, and (c) the convection heat transfer coefficient using Table 7-1.
What do you think about this solution?
We value your feedback to improve our textbook solutions.