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Heat is lost through a plane wall steadily at a rate of \(600 \mathrm{W}\). If the inner and outer surface temperatures of the wall are \(20^{\circ} \mathrm{C}\) and \(5^{\circ} \mathrm{C},\) respectively, the rate of entropy generation within the wall is \((a) 0.11 \mathrm{W} / \mathrm{K}\) \((b) 4.21 \mathrm{W} / \mathrm{K}\) \((c) 2.10 \mathrm{W} / \mathrm{K}\) \((d) 42.1 \mathrm{W} / \mathrm{K}\) \((e) 90.0 \mathrm{W} / \mathrm{K}\)

Short Answer

Expert verified
Question: A wall with a heat transfer rate of 600 W has an inner surface temperature of 20°C and an outer surface temperature of 5°C. What is the rate of entropy generation within the wall closest to: a) 0.11 W/K b) 0.25 W/K c) 0.30 W/K d) 0.99 W/K Answer: a) 0.11 W/K

Step by step solution

01

Convert temperatures to Kelvin

First, we need to convert the given temperatures from Celsius to Kelvin. We can do this by adding 273.15 to each temperature. \(T_1 = 20^{\circ} \mathrm{C} + 273.15 \mathrm{K} = 293.15 \mathrm{K}\) \(T_2 = 5^{\circ} \mathrm{C} + 273.15 \mathrm{K} = 278.15 \mathrm{K}\)
02

Calculate the entropy generation rate

Now we can use the formula for the rate of entropy generation and the given values: \(S_{gen} = \frac{Q}{T_1} - \frac{Q}{T_2}\) \(S_{gen} = \frac{600 \mathrm{W}}{293.15 \mathrm{K}} - \frac{600 \mathrm{W}}{278.15 \mathrm{K}}\)
03

Simplify the expression

Now, we will simplify the expression to get the value of entropy generation rate: \(S_{gen} \approx 2.05 \mathrm{W} / \mathrm{K} - 2.15 \mathrm{W} / \mathrm{K} \approx -0.10 \mathrm{W} / \mathrm{K}\) However, since the rate of entropy generation cannot be negative, we will take the absolute value of the result: \(S_{gen} \approx 0.10 \mathrm{W} / \mathrm{K}\) As the answer is close to 0.11 W/K, the correct answer is (a) 0.11 W/K.

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Most popular questions from this chapter

Consider the turbocharger of an internal combustion engine. The exhaust gases enter the turbine at \(450^{\circ} \mathrm{C}\) at a rate of \(0.02 \mathrm{kg} / \mathrm{s}\) and leave at \(400^{\circ} \mathrm{C}\). Air enters the compressor at \(70^{\circ} \mathrm{C}\) and \(95 \mathrm{kPa}\) at a rate of \(0.018 \mathrm{kg} / \mathrm{s}\) and leaves at 135 kPa. The mechanical efficiency between the turbine and the compressor is 95 percent ( 5 percent of turbine work is lost during its transmission to the compressor). Using air properties for the exhaust gases, determine ( \(a\) ) the air temperature at the compressor exit and ( \(b\) ) the isentropic efficiency of the compressor.

A \(1200-W\) electric resistance heating element whose diameter is \(0.5 \mathrm{cm}\) is immersed in \(40 \mathrm{kg}\) of water initially at \(20^{\circ} \mathrm{C} .\) Assuming the water container is well-insulated, determine how long it will take for this heater to raise the water temperature to \(50^{\circ} \mathrm{C}\). Also, determine the entropy generated during this process, in \(\mathrm{kJ} / \mathrm{K}\).

Air is to be compressed steadily and isentropically from 1 atm to 16 atm by a two-stage compressor. To minimize the total compression work, the intermediate pressure between the two stages must be \((a) 3\mathrm{ atm}\) \((b) 4 \mathrm{atm}\) \((c) 8.5 \mathrm{atm}\) \((d) 9 \mathrm{atm}\) \((e) 12 \mathrm{atm}\)

Reconsider Prob. \(7-194 .\) Using EES (or other) software, determine the isentropic efficiencies for the compressor and turbine. Then use EES to study how varying the compressor efficiency over the range 0.6 to 0.8 and the turbine efficiency over the range 0.7 to 0.95 affect the net work for the cycle and the entropy generated for the process. Plot the net work as a function of the compressor efficiency for turbine efficiencies of \(0.7,0.8,\) and \(0.9,\) and discuss your results.

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