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Oil at \(60^{\circ} \mathrm{C}\) flows at a velocity of $20 \mathrm{~cm} / \mathrm{s}\( over a \)5.0\(-m-long and \)1.0$-m-wide flat plate maintained at a constant temperature of \(20^{\circ} \mathrm{C}\). Determine the rate of heat transfer from the oil to the plate if the average oil properties are $\rho=880 \mathrm{~kg} / \mathrm{m}^{3}\(, \)\mu=0.005 \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, k=0.15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, and \)c_{p}=2.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}$.

Short Answer

Expert verified
Answer: The rate of heat transfer from the oil to the plate is 1314 W.

Step by step solution

01

Calculate the flow properties

We are given the temperature, flow velocity, and most of the fluid properties except the specific heat, \(c_{p}\). We can find it by converting it into the same unit as the other properties, which is given as: $$ c_{p} = 2.0 \times 10^3 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K} $$
02

Calculate the Reynolds number

The Reynolds number, \(Re\), is a dimensionless quantity that characterizes the flow regime. It can be calculated as: $$ Re = \frac{\rho u L}{\mu} $$ Where \(u\) is the flow velocity, \(L\) is the characteristic length (in this case, the length of the plate), and \(\rho\) and \(\mu\) are the density and dynamic viscosity of the oil, respectively. Using the given values, we find: $$ Re = \frac{880\,\mathrm{kg/m^3} \cdot 0.2\,\mathrm{m/s} \cdot 5\,\mathrm{m}}{0.005\,\mathrm{kg/m\cdot s}} = 176000 $$
03

Calculate the Nusselt number

The Nusselt number, \(Nu\), is another dimensionless quantity that relates the convective heat transfer coefficient to the thermal conductivity of the fluid. For laminar flow over a flat plate with constant wall temperature, the Nusselt number can be approximated by: $$ Nu = 0.664\,Re^{1/2}Pr^{1/3} $$ Where \(Pr\) is the Prandtl number, which is given by: $$ Pr=\frac{c_{p} \mu}{k} $$ Using the given fluid properties, we can calculate the Prandtl number as: $$ Pr = \frac{2\times 10^3\,\mathrm{J/kg\cdot K} \cdot 0.005\,\mathrm{kg/m\cdot s}}{0.15\,\mathrm{W/m\cdot K}} = 6.67 $$ And then calculate the Nusselt number: $$ Nu = 0.664 \times (176000)^{1/2} \times (6.67)^{1/3} = 219.1 $$
04

Calculate the convective heat transfer coefficient

The convective heat transfer coefficient, \(h\), can now be calculated using the Nusselt number: $$ h = \frac{Nu \times k}{L} = \frac{219.1 \times 0.15\,\mathrm{W/m\cdot K}}{5\,\mathrm{m}} = 6.57\,\mathrm{W/m^2\cdot K} $$
05

Compute the rate of heat transfer

Finally, we can calculate the rate of heat transfer, \(q\), using the convective heat transfer equation: $$ q = hA(T_\mathrm{fluid} - T_\mathrm{plate}) = 6.57\,\mathrm{W/m^2\cdot K} \times 5\,\mathrm{m} \times 1\,\mathrm{m} \times (60\,^{\circ}\mathrm{C} - 20\,^{\circ}\mathrm{C}) = 1314\,\mathrm{W} $$ So, the rate of heat transfer from the oil to the plate is 1314 W.

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Most popular questions from this chapter

Two metal plates are connected by a long ASTM A479 904L stainless steel bar. Air, at \(340^{\circ} \mathrm{C}\), flows at \(25 \mathrm{~m} / \mathrm{s}\) between the plates and across the bar. The bar has a square cross section with a width of \(10 \mathrm{~mm}\), and the length of the bar exposed to the hot air is \(10 \mathrm{~cm}\). The maximum use temperature for the ASTM A479 904L is \(260^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-1M). The temperature of the bar is maintained by a cooling mechanism capable of removing heat at a rate of \(50 \mathrm{~W}\). Determine whether the heat removed from the bar is sufficient to keep the bar at \(260^{\circ} \mathrm{C}\) or lower.

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 surface is (a) \(7383 \mathrm{~W}\) (b) \(8985 \mathrm{~W}\) (c) \(11,231 \mathrm{~W}\) (d) 14,672 W (e) 20,402 W (For air, use $k=0.02735 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7228, \nu=1.798 \times\( \)\left.10^{-5} \mathrm{~m}^{2} / \mathrm{s}\right)$

Hot engine oil at \(150^{\circ} \mathrm{C}\) is flowing in parallel over a flat plate at a velocity of \(2 \mathrm{~m} / \mathrm{s}\). Surface temperature of the \(0.5-\mathrm{m}\)-long flat plate is constant at \(50^{\circ} \mathrm{C}\). Determine (a) the local convection heat transfer coefficient at $0.2 \mathrm{~m}$ from the leading edge and the average convection heat transfer coefficient, and \((b)\) repeat part \((a)\) using the Churchill and Ozoe (1973) relation.

Air is to be cooled in the evaporator section of a refrigerator by passing it over a bank of \(0.8-\mathrm{cm}\)-outer-diameter and \(0.8-\mathrm{m}\)-long tubes inside which the refrigerant is evaporating at \(-20^{\circ} \mathrm{C}\). Air approaches the tube bank in the normal direction at \(0^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) with a mean velocity of \(5 \mathrm{~m} / \mathrm{s}\). The tubes are arranged in-line with longitudinal and transverse pitches of \(S_{L}=S_{T}=1.5 \mathrm{~cm}\). There are 25 rows in the flow direction with 15 tubes in each row. Determine \((a)\) the refrigeration capacity of this system and \((b)\) pressure drop across the tube bank. Evaluate the air properties at an assumed mean temperature of \(-5^{\circ} \mathrm{C}\) and $1 \mathrm{~atm}$. Is this a good assumption?

Air at \(15^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) flows over a \(0.3-\mathrm{m}\)-wide plate at \(65^{\circ} \mathrm{C}\) at a velocity of $3.0 \mathrm{~m} / \mathrm{s}$. Compute the following quantities at \(x=x_{\mathrm{cr}}\) : (a) Hydrodynamic boundary layer thickness, \(\mathrm{m}\) (b) Local friction coefficient (c) Average friction coefficient (d) Total drag force due to friction, \(\mathrm{N}\) (e) Local convection heat transfer coefficient, W/m² \(\mathrm{K}\) (f) Average convection heat transfer coefficient, W/m². \(\mathrm{K}\) (g) Rate of convective heat transfer, W

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