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Mercury at \(25^{\circ} \mathrm{C}\) flows over a 3 -m-long and 2 -m-wide flat plate maintained at \(75^{\circ} \mathrm{C}\) with a velocity of $0.01 \mathrm{~m} / \mathrm{s}$. Determine the rate of heat transfer from the entire plate.

Short Answer

Expert verified
Answer: The rate of heat transfer from the entire plate is approximately 2345.7 W.

Step by step solution

01

Calculate the Reynolds number

In this step, we'll calculate the Reynolds number to find the flow type on the plate. We will use the formula: $$Re = \frac{\rho VD}{\mu}$$, where \(\rho\) is the density of Mercury, \(V\) is the velocity, \(D\) is the characteristic length (for a flat plate, it's the length of the plate), and \(\mu\) is the dynamic viscosity of Mercury. At 25°C, Mercury properties are: \(\rho = 13400 ~kg/m^3\), \(\mu = 15.9 \times 10^{-4} ~Pa \cdot s\). The Reynolds number is: $$Re = \frac{(13400 ~kg/m^3)(0.01 ~m/s)(3 ~m)}{15.9 \times 10^{-4} ~Pa \cdot s} = 251.57$$ Since the Reynolds number is less than 5000, the flow is laminar.
02

Calculate the Nusselt number

For a flat plate with a laminar flow, the Nusselt number (Nu) can be calculated using the formula: $$Nu = 0.664 ~Re^{1/2} ~Pr^{1/3}$$, where Pr is the Prandtl number. The Prandtl number for Mercury is 0.0252. We already calculated the Reynolds number, Re=251.57. With these parameters, the Nusselt number is: $$Nu = 0.664(251.57)^{1/2}(0.0252)^{1/3} = 2.728$$
03

Calculate the heat transfer coefficient

By definition, the Nusselt number is the ratio of convective to the conductive heat transfer, which can be expressed as: $$Nu = \frac{hD}{k}$$, where \(k\) is the thermal conductivity of Mercury, which is \(8.55 ~W/(m \cdot K)\). We can solve for the heat transfer coefficient (h) using the values we calculated: $$h = \frac{k \cdot Nu}{D} = \frac{(8.55 ~W/(m \cdot K))(2.728)}{3 ~m} = 7.819 ~W/(m^2 \cdot K)$$
04

Calculate the rate of heat transfer

Now, we can calculate the rate of heat transfer using the formula: $$q = hA\Delta T$$, where \(A\) is the area (3 m length x 2 m width) and \(\Delta T\) is the temperature difference between the plate and Mercury (\(75^{\circ} \mathrm{C} - 25^{\circ} \mathrm{C} = 50^{\circ} \mathrm{C}\)). The rate of heat transfer is: $$q = (7.819 ~W/(m^2 \cdot K))(6 ~m^2)(50 ~K) = 2345.7 ~W$$ Thus, the rate of heat transfer from the entire plate is approximately 2345.7 W.

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Most popular questions from this chapter

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

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?

Consider a house that is maintained at a constant temperature of $22^{\circ} \mathrm{C}$. One of the walls of the house has three single-pane glass windows that are \(1.5 \mathrm{~m}\) high and \(1.8 \mathrm{~m}\) long. The glass $(k=0.78 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( is \)0.5 \mathrm{~cm}$ thick, and the heat transfer coefficient on the inner surface of the glass is $8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. Now winds at \)35 \mathrm{~km} / \mathrm{h}$ start to blow parallel to the surface of this wall. If the air temperature outside is \(-2^{\circ} \mathrm{C}\), determine the rate of heat loss through the windows of this wall. Assume radiation heat transfer to be negligible. Evaluate the air properties at a film temperature of $5^{\circ} \mathrm{C}\( and \)1 \mathrm{~atm}$.

Air $(k=0.028 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7)\( at \)50^{\circ} \mathrm{C}$ flows along a \(1-\mathrm{m}\)-long flat plate whose temperature is maintained at $20^{\circ} \mathrm{C}$ with a velocity such that the Reynolds number at the end of the plate is 10,000 . The heat transfer per unit width between the plate and air is (a) \(20 \mathrm{~W} / \mathrm{m}\) (b) \(30 \mathrm{~W} / \mathrm{m}\) (c) \(40 \mathrm{~W} / \mathrm{m}\) (d) \(50 \mathrm{~W} / \mathrm{m}\) (e) \(60 \mathrm{~W} / \mathrm{m}\)

Consider a hot automotive engine, which can be approximated as a \(0.5-\mathrm{m}\)-high, \(0.40\)-m-wide, and \(0.8\)-m-long rectangular block. The bottom surface of the block is at a temperature of \(100^{\circ} \mathrm{C}\) and has an emissivity of \(0.95\). The ambient air is at $20^{\circ} \mathrm{C}\(, and the road surface is at \)25^{\circ} \mathrm{C}$. Determine the rate of heat transfer from the bottom surface of the engine block by convection and radiation as the car travels at a velocity of $80 \mathrm{~km} / \mathrm{h}$. Assume the flow to be turbulent over the entire surface because of the constant agitation of the engine block.

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