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Heat flux meters use a very sensitive device known as a thermopile to measure the temperature difference across a thin, heat conducting film made of kapton \((k=0.345 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). If the thermopile can detect temperature differences of \(0.1^{\circ} \mathrm{C}\) or more and the film thickness is \(2 \mathrm{~mm}\), what is the minimum heat flux this meter can detect? A?swer: \(17.3 \mathrm{~W} / \mathrm{m}^{2}\)

Short Answer

Expert verified
Answer: The minimum detectable heat flux for this heat flux meter is 17.3 W/m².

Step by step solution

01

Convert the thickness to meters

Since the given thickness is in millimeters, we need to convert it to meters to maintain consistent units. We can do this by multiplying by the conversion factor (1 meter = 1000 millimeters): Thickness (m) = 2 mm * (1 m / 1000 mm) = 0.002 m
02

Re-write Fourier's Law with the known variables

Now, we can rewrite Fourier's Law using the given values for k and dT, and the converted value for dx: q = -0.345 W/m·K * (0.1°C / 0.002 m)
03

Calculate the minimum heat flux

Finally, we can calculate the minimum detectable heat flux by solving for q: q = -0.345 W/m·K * (0.1 K / 0.002 m) = 17.25 W/m² Since negative values indicate the direction of heat flux, we can present the result as a positive value: Minimum detectable heat flux = 17.3 W/m²

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Most popular questions from this chapter

Consider a solid cylindrical rod whose side surface is maintained at a constant temperature while the end surfaces are perfectly insulated. The thermal conductivity of the rod material is constant, and there is no heat generation. It is claimed that the temperature in the radial direction within the rod will not vary during steady heat conduction. Do you agree with this claim? Why?

A metal spherical tank is filled with chemicals undergoing an exothermic reaction. The reaction provides a uniform heat flux on the inner surface of the tank. The tank has an inner diameter of \(5 \mathrm{~m}\), and its wall thickness is \(10 \mathrm{~mm}\). The tank wall has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where $k_{0}=9.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \beta=0.0018 \mathrm{~K}^{-1}\(, and \)T$ is in \(\mathrm{K}\). The area surrounding the tank has an ambient temperature of \(15^{\circ} \mathrm{C}\), the tank's outer surface experiences convection heat transfer with a coefficient of \(80 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). Determine the heat flux on the tank's inner surface if the inner surface temperature is \(120^{\circ} \mathrm{C}\).

In subsea oil and natural gas production, hydrocarbon fluids may leave the reservoir with a temperature of \(70^{\circ} \mathrm{C}\) and flow in subsea surroundings of \(5^{\circ} \mathrm{C}\). Because of the temperature difference between the reservoir and the subsea environment, the knowledge of heat transfer is critical to prevent gas hydrate and wax deposition blockages. Consider a subsea pipeline with inner diameter of \(0.5 \mathrm{~m}\) and wall thickness of \(8 \mathrm{~mm}\) is used for transporting liquid hydrocarbon at an average temperature of \(70^{\circ} \mathrm{C}\), and the average convection heat transfer coefficient on the inner pipeline surface is estimated to be \(250 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The subsea has a temperature of \(5^{\circ} \mathrm{C}\), and the average convection heat transfer coefficient on the outer pipeline surface is estimated to be $150 \mathrm{~W} / \mathrm{m}^{2}\(. \)\mathrm{K}$. If the pipeline is made of material with thermal conductivity of $60 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, use the heat conduction equation to \)(a)$ obtain the temperature variation in the pipeline wall, \((b)\) determine the inner surface temperature of the pipeline, \((c)\) obtain the mathematical expression for the rate of heat loss from the liquid hydrocarbon in the pipeline, and \((d)\) determine the heat flux through the outer pipeline surface.

A flat-plate solar collector is used to heat water by having water flow through tubes attached at the back of the thin solar absorber plate. The absorber plate has an emissivity and an absorptivity of \(0.9\). The top surface \((x=0)\) temperature of the absorber is \(T_{0}=35^{\circ} \mathrm{C}\), and solar radiation is incident on the absorber at $500 \mathrm{~W} / \mathrm{m}^{2}\( with a surrounding temperature of \)0^{\circ} \mathrm{C}$. The convection heat transfer coefficient at the absorber surface is $5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, while the ambient temperature is \(25^{\circ} \mathrm{C}\). Show that the variation of temperature in the absorber plate can be expressed as $T(x)=-\left(\dot{q}_{0} / k\right) x+T_{0}\(, and determine net heat flux \)\dot{q}_{0}$ absorbed by the solar collector.

Liquid water flows in a tube with the inner surface lined with polyvinylidene chloride (PVDC). The inner diameter of the tube is \(24 \mathrm{~mm}\), and its wall thickness is \(5 \mathrm{~mm}\). The thermal conductivity of the tube wall is \(15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The water flowing in the tube has a temperature of \(20^{\circ} \mathrm{C}\), and the convection heat transfer coefficient with the inner tube surface is $50 \mathrm{~W} / \mathrm{m}^{2}\(. \)\mathrm{K}$. The outer surface of the tube is subjected to a uniform heat flux of \(2300 \mathrm{~W} / \mathrm{m}^{2}\). According to the ASME Code for Process Piping (ASME B31.3-2014, \(\mathrm{A} .323\) ), the recommended maximum temperature for PVDC lining is \(79^{\circ} \mathrm{C}\). Formulate the temperature profile in the tube wall. Use the temperature profile to determine if the tube inner surface is in compliance with the ASME Code for Process Piping.

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