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The forming section of a plastics plant puts out a continuous sheet of plastic that is \(1.2-\mathrm{m}\) wide and \(2-\mathrm{mm}\) thick at a rate of $15 \mathrm{~m} / \mathrm{min}$. The temperature of the plastic sheet is \(90^{\circ} \mathrm{C}\) when it is exposed to the surrounding air, and the sheet is subjected to airflow at \(30^{\circ} \mathrm{C}\) at a velocity of $3 \mathrm{~m} / \mathrm{s}$ on both sides along its surfaces normal to the direction of motion of the sheet. The width of the air cooling section is such that a fixed point on the plastic sheet passes through that section in $2 \mathrm{~s}$. Determine the rate of heat transfer from the plastic sheet to the air.

Short Answer

Expert verified
Answer: The rate of heat transfer from the plastic sheet to the air is approximately 14.4 W.

Step by step solution

01

Find the plastic sheet's surface area.

In order to determine the heat transfer rate, we first need to find the surface area of the plastic sheet. We know that the sheet is 1.2 meters wide and 2 mm thick. The equation for the area of a rectangle is A = length * width, so we find the surface area by multiplying the given dimensions: A = 1.2 m * 0.002 m = 0.0024 m^2 Since the plastic sheet has two sides, we multiply this result by 2 to get the total surface area: Total Surface Area = 0.0024 m^2 * 2 = 0.0048 m^2
02

Calculate the heat transfer coefficient.

To determine the heat transfer coefficient (h), we will use Newton's law of cooling, which states: q = hA(T_hot - T_cold) where q is the heat transfer rate, A is the surface area, T_hot is the temperature of the hot substance (in this case, the plastic sheet), and T_cold is the temperature of the surroundings (in this case, the airflow temperature). We are given T_hot as 90°C and T_cold as 30°C, so we can plug them into the equation: q = h * 0.0048 m^2 * (90°C - 30°C) We now need to find the heat transfer coefficient (h). Since there's no information given about the material properties, we can assume a value for h. In general, for forced convection, h ranges between 10 and 100 W/(m^2*K). We can assume h = 50 W/(m^2*K) as a reasonable approximation.
03

Calculate the rate of heat transfer.

With the heat transfer coefficient found in Step 2, we can now calculate the rate of heat transfer (q) by plugging in the values into the Newton's law of cooling equation: q = 50 W/(m^2*K) * 0.0048 m^2 * (90°C - 30°C) q = 50 W/(m^2*K) * 0.0048 m^2 * 60 K q = 14.4 W So, the rate of heat transfer from the plastic sheet to the air is approximately 14.4 W.

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Most popular questions from this chapter

In cryogenic equipment, cold air flows in parallel over the surface of a \(2-\mathrm{m} \times 2-\mathrm{m}\) ASTM A240 \(410 \mathrm{~S}\) stainless steel plate. The air velocity is \(5 \mathrm{~m} / \mathrm{s}\) at a temperature of \(-70^{\circ} \mathrm{C}\). The minimum temperature suitable for the ASTM A240 \(410 \mathrm{~S}\) plate is \(-30^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-1M). The plate is heated to keep its surface temperature from going below \(-30^{\circ} \mathrm{C}\). Determine the average heat transfer rate required to keep the plate surface from getting below the minimum suitable temperature.

Hydrogen gas at \(1 \mathrm{~atm}\) is flowing in parallel over the upper and lower surfaces of a 3 -m-long flat plate at a velocity of $2.5 \mathrm{~m} / \mathrm{s}\(. The gas temperature is \)120^{\circ} \mathrm{C}$, and the surface temperature of the plate is maintained at \(30^{\circ} \mathrm{C}\). Using appropriate software, investigate the local convection heat transfer coefficient and the local total convection heat flux along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient and the local total convection heat flux as functions of \(x\). Assume flow is laminar, but make sure to verify this assumption.

What is flow separation? What causes it? What is the effect of flow separation on the drag coefficient?

Repeat Prob. 7-137, assuming the inner surface of the tank to be at $0^{\circ} \mathrm{C}$ but by taking the thermal resistance of the tank and heat transfer by radiation into consideration. Assume the average surrounding surface temperature for radiation exchange to be \(25^{\circ} \mathrm{C}\) and the outer surface of the tank to have an emissivity of \(0.75\). Answers: (a) $379 \mathrm{~W}\(, (b) \)98.1 \mathrm{~kg}$

Engine oil at \(85^{\circ} \mathrm{C}\) flows over a \(10-\mathrm{m}\)-long flat plate whose temperature is \(35^{\circ} \mathrm{C}\) with a velocity of $2.5 \mathrm{~m} / \mathrm{s}$. Determine the total drag force and the rate of heat transfer over the entire plate per unit width.

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