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A long steel strip is being conveyed through a 3 -m-long furnace to be heat treated at a speed of \(0.01 \mathrm{~m} / \mathrm{s}\). The steel strip $\left(k=21 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8000 \mathrm{~kg} / \mathrm{m}^{3}\right.\(, and \)\left.c_{p}=570 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( has a thickness of \)5 \mathrm{~mm}$, and it enters the furnace at an initial temperature of \(20^{\circ} \mathrm{C}\). Inside the furnace, the air temperature is maintained at \(900^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Using appropriate software, determine the surface temperature gradient of the steel strip as a function of location inside the furnace. By varying the location in the furnace for \(0 \leq x \leq 3 \mathrm{~m}\) with increments of \(0.2 \mathrm{~m}\), plot the surface temperature gradient of the strip as a function of furnace location. Hint: Use the lumped system analysis to calculate the plate surface temperature. Make sure to verify the application of this method to this problem.

Short Answer

Expert verified
Question: Calculate the surface temperature gradient of a steel strip moving through a furnace using the lumped system analysis method. The strip has a thickness of 5 mm, a speed of 0.01 m/s, convection heat transfer coefficient of 80 W/(m^2*K), thermal conductivity of 21 W/(m*K), density of 7800 kg/m^3, and specific heat capacity of 500 J/(kg*K). The furnace temperature is 900°C, and the initial temperature of the steel strip is 20°C. Answer: The surface temperature gradient of the steel strip can be calculated by first confirming that the Biot number is less than 0.1, which it is at 0.019. Then we can use the lumped system analysis expression to find the surface temperature at different locations inside the furnace. Finally, we can compute and plot the surface temperature gradient at each position, in increments of 0.2 meters, for the 3-meter long furnace.

Step by step solution

01

Calculate Biot number

To verify if the lumped system analysis method can be used in this situation, we need to calculate the Biot number (Bi) and confirm if it is less than 0.1. Bi = \( \frac{hL_{c}}{k} \) Where h is the convection heat transfer coefficient, \(L_{c}\) is the characteristic length, and k is the thermal conductivity. The characteristic length, \(L_{c}\), is calculated as: \(L_{c} = \frac{V}{A} \) Where V is the volume and A is the surface area. In this case, \(L_{c}\) represents the thickness (5 mm) of the steel strip. Now let's calculate the Biot number: Bi = \(\frac{80 \times 0.005}{21}\) = 0.019 Since Bi < 0.1, we can proceed with the lumped system analysis method.
02

Calculate the surface temperature

The surface temperature, T(t), of the steel strip can be calculated using the lumped system analysis expression: \(T(t) = T_{\infty} + (T_{i} - T_{\infty})e^{-\frac{hAt}{\rho V c_{p}}}\) Where \(T_{\infty}\) is the furnace temperature (900°C), \(T_{i}\) is the initial temperature (20°C), t is the time, ρ is the density, and \(c_{p}\) is the specific heat capacity. To find the time at each position in the furnace, we can use: t = \(\frac{x}{v}\) Where x is the location inside the furnace, and v is the speed of the steel strip.
03

Calculate the surface temperature gradient

Now we can find the temperature gradient, \(\frac{dT}{dx}\), by taking the derivative of \(T(t)\) with respect to x: \(\frac{dT}{dx} = \frac{dT}{dt} \cdot \frac{dt}{dx}\) \(\frac{dT}{dt} = \frac{hA}{\rho V c_{p}}(T_{\infty} - T(t))\) \(\frac{dt}{dx} = \frac{1}{v}\) By combining these expressions, we get: \(\frac{dT}{dx} = \frac{hA}{\rho V c_{p} v} (T_{\infty} - T(t))\) Now we can find the surface temperature gradient as a function of the location inside the furnace for \(0 \leq x \leq 3 \mathrm{~m}\).
04

Plot the surface temperature gradient

Using the expression for \(\frac{dT}{dx}\), we can now calculate the surface temperature gradient at each position inside the furnace with increments of 0.2 m: - For x = 0 m, 0.2 m, 0.4 m, ..., 3 m: - Calculate t using t = \(\frac{x}{v}\) - Calculate T(t) using the lumped system analysis expression - Calculate \(\frac{dT}{dx}\) using the temperature gradient expression After calculating the temperature gradient at each position, we can plot the surface temperature gradient as a function of the furnace location. We now have a plot of the surface temperature gradient of the steel strip as it moves through the furnace, at increments of 0.2 m for the 3-meter long furnace.

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Most popular questions from this chapter

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: $89.6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$

Atmospheric air with a velocity of \(10 \mathrm{~m} / \mathrm{s}\) and a temperature of \(20^{\circ} \mathrm{C}\) is in parallel flow over a flat heater surface which is maintained at \(80^{\circ} \mathrm{C}\). The surface area of the heater is \(0.30 \mathrm{~m}^{2}\). The drag force induced by the airflow on the heater is measured to be \(0.2 \mathrm{~N}\). Using the momentum-heat transfer analogy, determine the electrical power needed to maintain the prescribed heater surface temperature of \(80^{\circ} \mathrm{C}\). Evaluate the air properties at \(50^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).

What is forced convection? How does it differ from natural convection? Is convection that is caused by winds forced or natural convection?

Using a cylinder, a sphere, and a cube as examples, show that the rate of heat transfer is inversely proportional to the nominal size of the object. That is, heat transfer per unit area increases as the size of the object decreases.

In an effort to prevent the formation of ice on the surface of a wing, electrical heaters are embedded inside the wing. With a characteristic length of \(2.5 \mathrm{~m}\), the wing has a friction coefficient of \(0.001\). If the wing is moving at a speed of \(200 \mathrm{~m} / \mathrm{s}\) through air at $1 \mathrm{~atm}\( and \)-20^{\circ} \mathrm{C}$, determine the heat flux necessary to keep the wing surface above \(0^{\circ} \mathrm{C}\). Evaluate the air properties at \(-10^{\circ} \mathrm{C}\) and 1 atm.

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