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An average man has a body surface area of \(1.8 \mathrm{~m}^{2}\) and a skin temperature of \(33^{\circ} \mathrm{C}\). The convection heat transfer coefficient for a clothed person walking in still air is expressed as $h=8.6 V^{0.53}\( for \)0.5

Short Answer

Expert verified
Answer: To find the rate of heat loss for each walking velocity, first calculate the convection heat transfer coefficient (h) using the formula \(h = 8.6 V^{0.53}\) for each velocity (V). Next, use the heat transfer equation \(q = hA(T_{s} - T_{\infty})\) with the calculated h values and given surface area (A), surface temperature (\(T_{s}\)), and air temperature (\(T_{\infty}\)) to determine the rate of heat loss (q) for each walking velocity.

Step by step solution

01

Define known parameters

In this problem, we are given the body surface area (A = 1.8 m²), air temperature (\(T_{\infty}\) = 7°C), and surface temperature (\(T_{s}\) = 30°C).
02

Calculate the convection heat transfer coefficient (h)

Having the given formula for the convection heat transfer coefficient: \(h = 8.6 V^{0.53}\), we will calculate h for each walking velocity: (a) 0.5 m/s, (b) 1 m/s, (c) 1.5 m/s, (d) 2 m/s.
03

Calculate the rate of heat loss q

Now, we will use the formula \(q = hA(T_{s} - T_{\infty})\) to calculate the rate of heat loss for each walking velocity using the calculated h values from step 2. 3a. For \(V = 0.5\) m/s: Calculate h: \(h = 8.6 (0.5)^{0.53}\) Then calculate q: \(q = h(1.8)(30 - 7)\) 3b. For \(V = 1.0\) m/s: Calculate h: \(h = 8.6 (1)^{0.53}\) Then calculate q: \(q=h(1.8)(30-7)\) 3c. For \(V = 1.5\) m/s: Calculate h: \(h = 8.6 (1.5)^{0.53}\) Then calculate q: \(q=h(1.8)(30-7)\) 3d. For \(V = 2.0\) m/s: Calculate h: \(h = 8.6 (2)^{0.53}\) Then calculate q: \(q=h(1.8)(30-7)\) After calculating the rate of heat loss (q) for each walking velocity in step 3, we have found the solution for each part of this exercise.

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Most popular questions from this chapter

The upper surface of a \(1-\mathrm{m} \times 1-\mathrm{m}\) ASTM B 152 copper plate is being cooled by air at \(20^{\circ} \mathrm{C}\). The air is flowing parallel over the plate surface at a velocity of $0.5 \mathrm{~m} / \mathrm{s}$. The local convection heat transfer coefficient along the plate surface is correlated with the correlation \(h_{x}=1.36 x^{-0.5}\), where \(h_{x}\) and \(x\) have the units \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(\mathrm{m}\), respectively. The maximum use temperature for the ASTM B152 copper plate is \(260^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-1M). Evaluate the average convection heat transfer coefficient \(h\) for the entire plate. If the rate of convection heat transfer from the plate surface is \(700 \mathrm{~W}\), would the use of ASTM B152 plate be in compliance with the ASME Code for Process Piping?

Consider steady, laminar, two-dimensional flow over an isothermal plate. Does the wall shear stress increase, decrease, or remain constant with distance from the leading edge?

Two metal plates are connected by a long ASTM B 98 copper-silicon bolt. A hot gas at \(200^{\circ} \mathrm{C}\) flows between the plates and across the cylindrical bolt. The diameter of the bolt is \(9.5 \mathrm{~mm}\), and the length of the bolt exposed to the hot gas is \(10 \mathrm{~cm}\). The average convection heat transfer coefficient for the bolt in crossflow is correlated with the gas velocity as \(h=24.6 \mathrm{~V}^{0.62}\), where \(h\) and \(V\) have the units \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and $\mathrm{m} / \mathrm{s}$, respectively. The maximum use temperature for the ASTM B98 bolt is \(149^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-2M). If the gas velocity is \(10.4 \mathrm{~m} / \mathrm{s}\), determine the minimum heat removal rate required to keep the bolt surface from going above the maximum use temperature.

What is turbulent viscosity? What is it caused by?

Consider an airplane cruising at an altitude of \(10 \mathrm{~km}\) where standard atmospheric conditions are \(-50^{\circ} \mathrm{C}\) and $26.5 \mathrm{kPa}\( at a speed of \)800 \mathrm{~km} / \mathrm{h}$. Each wing of the airplane can be modeled as a \(25-\mathrm{m} \times 3-\mathrm{m}\) flat plate, and the friction coefficient of the wings is \(0.0016\). Using the momentum-heat transfer analogy, determine the heat transfer coefficient for the wings at cruising conditions. Answer: $89.6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$

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