Hydrogen gas at \(1 \mathrm{~atm}\) is flowing in parallel over the upper and lower surfaces of a 3-m-long flat plate at a velocity of \(2.5 \mathrm{~m} / \mathrm{s}\). The gas temperature is \(120^{\circ} \mathrm{C}\) and the surface temperature of the plate is maintained at \(30^{\circ} \mathrm{C}\). Using the EES (or other) software, investigate the local convection heat transfer coefficient and the local total convection heat flux along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient and the local total convection heat flux as functions of \(x\). Assume flow is laminar but make sure to verify this assumption. 7-31 Carbon dioxide and hydrogen as ideal gases at \(1 \mathrm{~atm}\) and \(-20^{\circ} \mathrm{C}\) flow in parallel over a flat plate. The flow velocity of each gas is \(1 \mathrm{~m} / \mathrm{s}\) and the surface temperature of the 3 -m-long plate is maintained at \(20^{\circ} \mathrm{C}\). Using the EES (or other) software, evaluate the local Reynolds number, the local Nusselt number, and the local convection heat transfer coefficient along the plate for each gas. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local Reynolds number, the local Nusselt number, and the local convection heat transfer coefficient for each gas as functions of \(x\). Discuss which gas has higher local Nusselt number and which gas has higher convection heat transfer coefficient along the plate. Assume flow is laminar but make sure to verify this assumption.

Short Answer

Expert verified
Question: Calculate the local convection heat transfer coefficient and local total convection heat flux along a 3m-long flat plate for hydrogen gas flowing in parallel at specific conditions, and plot them as functions of x, considering laminar flow. Also, evaluate the local Reynolds number, the local Nusselt number, and the local convection heat transfer coefficient for carbon dioxide and hydrogen gases with given conditions, and plot them as functions of x. Discuss which gas has a higher local Nusselt number and convection heat transfer coefficient.

Step by step solution

01

1. Calculations for Hydrogen gas

First, we need to calculate the local convection heat transfer coefficient by knowing basic properties such as thermal conductivity, dynamic viscosity, and heat capacity of hydrogen gas at given temperatures. It's necessary to determine the flow regime (laminar or turbulent) by calculating the Reynolds number. Reynolds number, \(Re = \frac{V \cdot x}{\nu}\) If the Reynolds number is less than 5 x 10^5 (Re < 5 x 10^5), we can consider the flow to be laminar. For laminar flow, we can use the following relation to compute the local Nusselt number: Local Nusselt number, \(Nu = 0.332 Re^{\frac{1}{2}} Pr^{\frac{1}{3}}\) The local convection heat transfer coefficient can be calculated using: Local convection heat transfer coefficient, \(h = \frac{k \cdot Nu}{x}\) Once we have the local convection heat transfer coefficient, we can use it to calculate the local total convection heat flux: \(Local convection heat flux = h \cdot A \cdot \Delta T\) where \(A = width \cdot x\) and \(\Delta T = T_\text{surface} - T_\text{gas}\).
02

2. Plotting Hydrogen gas results

Next, we need to plot these quantities as functions of x for hydrogen gas. We should vary the location along the plate (\(0.2 \leq x \leq 3 \mathrm{~m}\)) and create a plot for the local convection heat transfer coefficient and local total convection heat flux.
03

3. Calculations for Carbon Dioxide and Hydrogen gases

Next, we need to repeat the calculations (Reynolds number, Nusselt number, and convection heat transfer coefficient) for carbon dioxide and hydrogen gases at the given conditions. We need to determine and verify if the flow is laminar for both gases, and again, we have to use the laminar flow equation for the local Nusselt number.
04

4. Plotting CO₂ and H₂ results

Once we have the results for carbon dioxide and hydrogen gases, we need to plot the local Reynolds number, local Nusselt number, and local convection heat transfer coefficient as functions of x for each gas.
05

5. Discussion

Finally, based on the plotted results for both gases, we need to discuss which gas has a higher local Nusselt number and convection heat transfer coefficient along the 3-meter-long flat plate.

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Most popular questions from this chapter

To defrost ice accumulated on the outer surface of an automobile windshield, warm air is blown over the inner surface of the windshield. Consider an automobile windshield \(\left(k_{w}=1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) with an overall height of \(0.5 \mathrm{~m}\) and thickness of \(5 \mathrm{~mm}\). The outside air ( \(1 \mathrm{~atm}\) ) ambient temperature is \(-20^{\circ} \mathrm{C}\) and the average airflow velocity over the outer windshield surface is \(80 \mathrm{~km} / \mathrm{h}\), while the ambient temperature inside the automobile is \(25^{\circ} \mathrm{C}\). Determine the value of the convection heat transfer coefficient, for the warm air blowing over the inner surface of the windshield, necessary to cause the accumulated ice to begin melting. Assume the windshield surface can be treated as a flat plate surface.

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A glass \((k=1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) spherical tank is filled with chemicals undergoing exothermic reaction. The reaction keeps the inner surface temperature of the tank at \(80^{\circ} \mathrm{C}\). The tank has an inner radius of \(0.5 \mathrm{~m}\) and its wall thickness is \(10 \mathrm{~mm}\). Situated in surroundings with an ambient temperature of \(15^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of \(70 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), the tank's outer surface is being cooled by air flowing across it at \(5 \mathrm{~m} / \mathrm{s}\). In order to prevent thermal burn on individuals working around the container, it is necessary to keep the tank's outer surface temperature below \(50^{\circ} \mathrm{C}\). Determine whether or not the tank's outer surface temperature is safe from thermal burn hazards.

Wind at \(30^{\circ} \mathrm{C}\) flows over a \(0.5\)-m-diameter spherical tank containing iced water at \(0^{\circ} \mathrm{C}\) with a velocity of \(25 \mathrm{~km} / \mathrm{h}\). If the tank is thin-shelled with a high thermal conductivity material, the rate at which ice melts is (a) \(4.78 \mathrm{~kg} / \mathrm{h} \quad\) (b) \(6.15 \mathrm{~kg} / \mathrm{h}\) (c) \(7.45 \mathrm{~kg} / \mathrm{h}\) (d) \(11.8 \mathrm{~kg} / \mathrm{h}\) (e) \(16.0 \mathrm{~kg} / \mathrm{h}\) (Take \(h_{i f}=333.7 \mathrm{~kJ} / \mathrm{kg}\), and use the following for air: \(k=\) \(0.02588 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7282, v=1.608 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, \mu_{\infty}=\) \(\left.1.872 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, \mu_{\mathrm{s}}=1.729 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\right)\)

Airstream at 1 atm flows, with a velocity of \(15 \mathrm{~m} / \mathrm{s}\), in parallel over a 3-m-long flat plate where there is an unheated starting length of \(1 \mathrm{~m}\). The airstream has a temperature of \(20^{\circ} \mathrm{C}\) and the heated section of the flat plate is maintained at a constant temperature of \(80^{\circ} \mathrm{C}\). Determine \((a)\) the local convection heat transfer coefficient at the trailing edge and (b) the average convection heat transfer coefficient for the heated section.

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