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How would the answer to Prob. 11-150 be altered if we tried to approximate the heat transfer loss through the blood vessel with a fouling factor to describe physiological inhomogeneities? Assume that the fouling factor for the artery is \(0.0005\) \(\mathrm{m}^{2}\). K/W and the fouling factor for the vein is \(0.0003 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\).

Short Answer

Expert verified
Answer: The inclusion of fouling factors for the artery and vein increases the overall resistance to heat transfer, resulting in a lower heat transfer rate compared to the original calculation in Prob. 11-150. This demonstrates how physiological inhomogeneities can impact heat transfer loss through blood vessels.

Step by step solution

01

Understand the fouling factor

The fouling factor is a measure of the resistance to heat transfer caused by deposition or buildup of impurities or unwanted materials on heat transfer surfaces. The higher the fouling factor, the lower the overall heat transfer rate. In this exercise, we are given a fouling factor for both the artery and the vein. Including the fouling factor should thus increase the overall resistance and reduce the heat transfer rate.
02

Calculate the total resistance considering the fouling factors

First, the overall resistance for both the artery and vein WITHOUT fouling factors (denoted R1 and R2 respectively) should have been calculated in Prob. 11-150 using formulas from heat transfer. Now, we have to include the fouling factors in these resistances. We can do this by adding the fouling factor values directly to the calculated resistances for each blood vessel. Let \(R1^*\) and \(R2^*\) be the modified resistances for the artery and vein, including the fouling factors: $$R1^* = R1 + 0.0005 \mathrm{~m}^{-2} \cdot \mathrm{K} / \mathrm{W}$$ $$R2^* = R2 + 0.0003 \mathrm{~m}^{-2} \cdot \mathrm{K} / \mathrm{W}$$
03

Calculate the new overall heat transfer rate

To find the altered heat transfer rate, we need to use the formula for heat transfer considering the modified resistances \(R1^*\) and \(R2^*\), $$Q = \frac{(\Delta T)} {R_{total}}$$ where \(Q\) represents the heat transfer rate, \(\Delta T\) is the temperature difference between the artery and vein, and \(R_{total}\) is the total resistance in the system, which can be calculated as: $$R_{total} = R1^* + R2^*$$ Since we have already calculated \(R1^*\) and \(R2^*\) in Step 2, we can substitute these values in the equation above to find the new total resistance. Then, by combining this with the temperature difference between the artery and vein, which was provided in Prob. 11-150, we can determine the new heat transfer rate.
04

Compare the new and old heat transfer rates

Finally, we should compare the new heat transfer rate (calculated with the fouling factors) to the original heat transfer rate (calculated in Prob. 11-150). This will help us understand how the answer to Prob. 11-150 is altered when the fouling factors are considered. The difference between the two heat transfer rates will indicate the impact of physiological inhomogeneities on heat transfer loss through the blood vessel. In conclusion, by considering the fouling factors for the artery and vein, we can find the new overall resistance, and thus the new heat transfer rate, which would be lower than originally calculated in Prob. 11-150. This shows how including the fouling factors for physiological inhomogeneities would alter the answer to the original problem.

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Most popular questions from this chapter

The cardiovascular countercurrent heat exchanger has an overall heat transfer coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Arterial blood enters at \(37^{\circ} \mathrm{C}\) and exits at \(27^{\circ} \mathrm{C}\). Venous blood enters at \(25^{\circ} \mathrm{C}\) and exits at $34^{\circ} \mathrm{C}$. Determine the mass flow rates of the arterial blood and venous blood in \(\mathrm{g} / \mathrm{s}\) if the specific heat of both arterial and venous blood is constant and equal to $3475 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\(, and the surface area of the heat transfer to occur is \)0.15 \mathrm{~cm}^{2}$.

The radiator in an automobile is a crossflow heat exchanger $\left(U A_{s}=10 \mathrm{~kW} / \mathrm{K}\right)\( that uses air \)\left(c_{p}=1.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)$ to cool the engine coolant fluid \(\left(c_{p}=4.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\). The engine fan draws \(30^{\circ} \mathrm{C}\) air through this radiator at a rate of \(12 \mathrm{~kg} / \mathrm{s}\) while the coolant pump circulates the engine coolant at a rate of \(5 \mathrm{~kg} / \mathrm{s}\). The coolant enters this radiator at \(80^{\circ} \mathrm{C}\). Under these conditions, what is the number of transfer units (NTU) of this radiator? (a) \(2.0\) (b) \(2.5\) (c) \(3.0\) (d) \(3.5\) (e) \(4.0\)

Consider a recuperative crossflow heat exchanger (both fluids unmixed) used in a gas turbine system that carries the exhaust gases at a flow rate of $7.5 \mathrm{~kg} / \mathrm{s}\( and a temperature of \)500^{\circ} \mathrm{C}$. The air initially at \(30^{\circ} \mathrm{C}\) and flowing at a rate of $15 \mathrm{~kg} / \mathrm{s}$ is to be heated in the recuperator. The convective heat transfer coefficients on the exhaust gas and air sides are $750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)300 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$, respectively. Due to long-term use of the gas turbine, the recuperative heat exchanger is subject to fouling on both gas and air sides that offers a resistance of \(0.0004\) \(\mathrm{m}^{2}\). $/ \mathrm{W}$ each. Take the properties of exhaust gas to be the same as that of air \(\left(c_{p}=1069 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\). If the exit temperature of the exhaust gas is \(320^{\circ} \mathrm{C}\), determine \((a)\) if the air could be heated to a temperature of \(150^{\circ} \mathrm{C}\) and \((b)\) the area of the heat exchanger. (c) If the answer to part \((a)\) is no, then determine what should be the air mass flow rate in order to attain the desired exit temperature of \(150^{\circ} \mathrm{C}\) and \((d)\) plot the variation of the exit air temperature over a range of \(75^{\circ} \mathrm{C}\) to \(300^{\circ} \mathrm{C}\) with the air mass flow rate, assuming all the other conditions remain the same.

Hot oil \(\left(c_{p}=2.1 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(110^{\circ} \mathrm{C}\) and \(12 \mathrm{~kg} / \mathrm{s}\) is to be cooled in a heat exchanger by cold water \(\left(c_{p}=4.18\right.\) $\mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K})\( entering at \)10^{\circ} \mathrm{C}$ and at a rate of \(2 \mathrm{~kg} / \mathrm{s}\). The lowest temperature that oil can be cooled in this heat exchanger is (a) \(10^{\circ} \mathrm{C}\) (b) \(24^{\circ} \mathrm{C}\) (c) \(47^{\circ} \mathrm{C}\) (d) \(61^{\circ} \mathrm{C}\) (e) \(77^{\circ} \mathrm{C}\)

A heat exchanger is to cool oil $\left(c_{p}=2200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( at a rate of \)10 \mathrm{~kg} / \mathrm{s}$ from \(120^{\circ} \mathrm{C}\) to \(40^{\circ} \mathrm{C}\) by air. Determine the heat transfer rating of the heat exchanger and propose a suitable type.

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