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For laminar flow over a flat plate, the local heat transfer coefficient varies as \(h_{x}=C x^{-0.5}\), where \(x\) is measured from the leading edge of the plate and \(C\) is a constant. Determine the ratio of the average convection heat transfer coefficient over the entire plate of length \(L\) to the local convection heat transfer coefficient at the end of the plate.

Short Answer

Expert verified
Answer: The ratio between the average convection heat transfer coefficient over the entire plate length and the local heat transfer coefficient at the end of the plate is 2.

Step by step solution

01

Determine the average heat transfer coefficient over the entire plate length

First, we need to determine the average convection heat transfer coefficient (\(\overline{h}\)) over the entire length of the plate, which can be found by integrating the given function of \(h(x)\) with respect to \(x\), and then dividing this result by the length of the plate. This can be expressed as: $$ \overline{h} = \frac{1}{L} \int_0^L h_x dx = \frac{1}{L} \int_0^L C x^{-0.5} dx $$ We can now find this integral and obtain the value for the average heat transfer coefficient.
02

Integrate the heat transfer coefficient function

Integrating the given function of \(h_x\) with respect to \(x\) gives the following result: $$ \int_0^L C x^{-0.5} dx = C \int_0^L x^{-0.5} dx = 2C \left[x^{0.5}\right]_0^L = 2CL^{0.5} $$
03

Calculate the average heat transfer coefficient

Plugging the result of the integral back into the equation for the average heat transfer coefficient, we can find the value for \(\overline{h}\): $$ \overline{h} = \frac{1}{L} (2CL^{0.5}) = 2C L^{-0.5} $$
04

Find the local heat transfer coefficient at x=L

The local heat transfer coefficient at the end of the plate, \(h_L\), is given by the same function \(h_x\), and we need to plug in \(x=L\) to find its value: $$ h_L = C L^{-0.5} $$
05

Determine the ratio of average to local heat transfer coefficients

Now that we have calculated both the average and local heat transfer coefficients, we can find the ratio of \(\overline{h}\) to \(h_L\). We can do that by dividing \(\overline{h}\) by \(h_L\) as follows: $$ \frac{\overline{h}}{h_L} = \frac{2C L^{-0.5}}{C L^{-0.5}}=2 $$ Thus, the ratio between the average convection heat transfer coefficient over the entire plate length and the local heat transfer coefficient at the end of the plate is 2.

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Most popular questions from this chapter

What is turbulent thermal conductivity? What is it caused by?

Consider steady, laminar, two-dimensional, incompressible flow with constant properties and a Prandtl number of unity. For a given geometry, is it correct to say that both the average friction and heat transfer coefficients depend on the Reynolds number only?

Consider airflow over a plate surface maintained at a temperature of \(220^{\circ} \mathrm{C}\). The temperature profile of the airflow is given as $$ T(y)=T_{\infty}-\left(T_{\infty}-T_{s}\right) \exp \left(-\frac{V}{\alpha_{\text {faid }}} y\right) $$ The airflow at 1 atm has a free stream velocity and temperature of $0.08 \mathrm{~m} / \mathrm{s}\( and \)20^{\circ} \mathrm{C}$, respectively. Determine the heat flux on the plate surface and the convection heat transfer coefficient of the airflow.

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.

A metallic airfoil of elliptical cross section has a mass of $50 \mathrm{~kg}\(, surface area of \)12 \mathrm{~m}^{2}$, and a specific heat of \(0.50 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\). The airfoil is subjected to airflow at \(1 \mathrm{~atm}\), \(25^{\circ} \mathrm{C}\), and $5 \mathrm{~m} / \mathrm{s}$ along its 3 -m-long side. The average temperature of the airfoil is observed to drop from \(160^{\circ} \mathrm{C}\) to \(150^{\circ} \mathrm{C}\) within 2 min of cooling. Assuming the surface temperature of the airfoil to be equal to its average temperature and using the momentum-heat transfer analogy, determine the average friction coefficient of the airfoil surface. Evaluate the air properties at \(25^{\circ} \mathrm{C}\) and 1 atm. Answer: \(0.000363\)

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