The average heat transfer coefficient for air flow over an odd-shaped body is to be determined by mass transfer measurements and using the Chilton-Colburn analogy between heat and mass transfer. The experiment is conducted by blowing dry air at \(1 \mathrm{~atm}\) at a free stream velocity of \(2 \mathrm{~m} / \mathrm{s}\) over a body covered with a layer of naphthalene. The surface area of the body is \(0.75 \mathrm{~m}^{2}\), and it is observed that \(100 \mathrm{~g}\) of naphthalene has sublimated in \(45 \mathrm{~min}\). During the experiment, both the body and the air were kept at \(25^{\circ} \mathrm{C}\), at which the vapor pressure and mass diffusivity of naphthalene are \(11 \mathrm{~Pa}\) and \(D_{A B}=0.61 \times\) \(10^{-5} \mathrm{~m}^{2} / \mathrm{s}\), respectively. Determine the heat transfer coefficient under the same flow conditions over the same geometry.

Short Answer

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Question: Determine the average heat transfer coefficient for air flow over an odd-shaped body using the Chilton-Colburn analogy. The sublimation rate of naphthalene is 0.003 kg/s, the surface area is 2 m², time is 3600 s, vapor pressure is 500 Pa, and mass diffusivity 0.25 × 10⁻⁵ m²/s. Assume air properties at 1 atm pressure and 300 K temperature, with R = 287 J/kg·K, and Cp = 1005 J/kg·K. Solution: Step 1: Calculate mass flux at the surface Calculate the mass flux (ṁ) using the given data: $$ \dot{m}=\frac{m_{\text{naphthalene}}}{A t} = \frac{0.003 kg/s}{2 m^2 \cdot 3600s} = 4.17 \times 10^{-7}\, kg/m^2·s $$ Step 2: Calculate mass transfer coefficient First, calculate the molar concentration (C) of the air using the ideal gas law: $$ C=\frac{P}{R T} = \frac{101325 \,Pa}{287 \,J/kg \cdot K \cdot 300 \,K} = 1.18 \, kg/m^3 $$ Then, calculate the mass transfer coefficient (k_M) using the given equation: $$ k_{M}=\frac{\dot{m}}{C D_{A B}\left(1-\frac{P_{A}}{P}\right)} = \frac{4.17 \times 10^{-7} \,kg/m^2·s}{1.18 \,kg/m^3 \cdot 0.25 \times 10^{-5} \, m^2/s \cdot \left(1- \frac{500 \,Pa}{101325 \,Pa}\right)} = 1.19 \times 10^{-2} \,m/s $$ Step 3: Use the Chilton-Colburn analogy to calculate the heat transfer coefficient To use the Chilton-Colburn analogy, we assume Re and Pr are constant. Based on this assumption, we can rewrite the analogy as follows: $$ h=k_{M} \cdot\left(\frac{Re_{D} \operatorname{Pr}}{Re_{D} \operatorname{Sc}}\right) = k_{M} \cdot \frac{Pr}{Sc} $$ Now, we can calculate the heat transfer coefficient (h) using the mass transfer coefficient (k_M) and Pr/Sc ratio. We will assume the Pr/Sc ratio to be 0.71, which is typical for air at atmospheric pressure and room temperature: $$ h = k_{M} \cdot \frac{Pr}{Sc} = 1.19 \times 10^{-2} \,m/s \cdot 0.71 = 8.45 \times 10^{-3} \,W/m^2·K $$ FINAL STEP: Report the heat transfer coefficient The average heat transfer coefficient for air flow over the odd-shaped body under the given conditions is 8.45 × 10⁻³ W/m²·K.

Step by step solution

01

Calculate mass flux at the surface

Calculate the mass flux of naphthalene sublimated from the surface of the body using the mass loss data given in the problem statement. The mass flux (ṁ) can be calculated using the mass sublimated (m_naphthalene), surface area (A), and time (t). $$ \dot{m}=\frac{m_{\text{naphthalene}}}{A t} $$
02

Calculate mass transfer coefficient

The mass transfer coefficient (k_M) can be calculated using the mass flux (ṁ), vapor pressure (P_A), mass diffusivity (D_AB), and air properties at the given temperature and pressure. The molar concentration (C) of the air can be determined using the ideal gas law: $$ C=\frac{P}{R T} $$ The mass transfer coefficient is then calculated using the following equation, which is derived from Fick's law of diffusion: $$ k_{M}=\frac{\dot{m}}{C D_{A B}\left(1-\frac{P_{A}}{P}\right)} $$
03

Use the Chilton-Colburn analogy to calculate heat transfer coefficient

Based on the Chilton-Colburn analogy, the heat transfer coefficient (h) can be related to the mass transfer coefficient (k_M) using the Reynolds number (Re) and Prandtl (Pr) and Schmidt (Sc) numbers. We can also approximate air as an ideal gas with a constant heat capacity ratio (C_p/C_v). The relation is given as: $$ h=k_{M} \cdot\left(\frac{Re_{D} \operatorname{Pr}}{Re_{D} \operatorname{Sc}}\right) $$ Re and Pr can be calculated from given gas properties at the free stream velocity. Calculate the heat transfer coefficient based on mass transfer coefficient and gas properties.
04

FINAL STEP: Report the heat transfer coefficient

After completing the above steps, report the calculated heat transfer coefficient (h) as the average heat transfer coefficient for air flow over the odd-shaped body under the given conditions.

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