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The upper surface of an ASME SB-96 coppersilicon plate is subjected to convection with hot air flowing at \(7.5 \mathrm{~m} / \mathrm{s}\) parallel over the plate surface. The length of the plate is \(1 \mathrm{~m}\), and the temperature of the hot air is \(200^{\circ} \mathrm{C}\). The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits equipment constructed with ASME SB-96 plate to be operated at a temperature not exceeding \(93^{\circ} \mathrm{C}\). In the interest of designing a cooling mechanism to keep the plate surface temperature from exceeding \(93^{\circ} \mathrm{C}\), determine the variation of the local heat flux on the plate surface for $0

Short Answer

Expert verified
The formula used to calculate the local heat flux on the ASME SB-96 coppersilicon plate in terms of the local heat transfer coefficient is: $$q_x = h_x (T_{air} - T_{plate})$$ where \(q_x\) is the local heat flux, \(h_x\) is the local heat transfer coefficient, \(T_{air}\) is the temperature of the hot air, and \(T_{plate}\) is the temperature of the plate, which must not exceed 93°C.

Step by step solution

01

Calculate Reynolds number

To calculate the Reynolds number, we can use the formula: $$Re_x = \frac{\rho v x}{\mu}$$ where Re_x is the local Reynolds number, \(\rho\) is the air density, v is the air velocity, x is the distance along the plate, and \(\mu\) is the air dynamic viscosity. #Step 2: Calculate Prandtl number#
02

Calculate Prandtl number

To calculate the Prandtl number, we can use the formula: $$Pr = \frac{c_p \mu}{k}$$ where Pr is the Prandtl number, \(c_p\) is the specific heat capacity at constant pressure, \(\mu\) is the air dynamic viscosity, and k is the air thermal conductivity. #Step 3: Calculate local Nusselt number using correlation for a flat plate#
03

Calculate local Nusselt number

We can use the following correlation for the local Nusselt number for a flat plate: $$Nu_x = (0.037Re_x^{4/5} - 871) Pr^{1/3}$$ #Step 4: Calculate local heat transfer coefficient#
04

Calculate local heat transfer coefficient

We can now find the local heat transfer coefficient using the formula: $$h_x = \frac{Nu_x k}{x}$$ where \(h_x\) is the local heat transfer coefficient and \(Nu_x\) is the local Nusselt number. #Step 5: Calculate local heat flux using the local heat transfer coefficient#
05

Calculate local heat flux

We can calculate the local heat flux using the formula: $$q_x = h_x (T_{air} - T_{plate})$$ where \(q_x\) is the local heat flux, \(h_x\) is the local heat transfer coefficient, \(T_{air}\) is the temperature of the hot air, and \(T_{plate}\) is the temperature of the plate, which must not exceed 93°C. #Step 6: Plot the local heat flux on the plate surface#
06

Plot the local heat flux

Now we will plot the local heat flux on the plate surface for \(0 \leq x \leq 1 \mathrm{~m}\). Using the formulas discussed in the previous steps, we can calculate the local heat flux values for different x values and plot these on a graph.

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Most popular questions from this chapter

What does the friction coefficient represent in flow over a flat plate? How is it related to the drag force acting on the plate?

A \(5-\mathrm{m} \times 5-\mathrm{m}\) flat plate maintained at a constant temperature of \(80^{\circ} \mathrm{C}\) is subjected to parallel flow of air at \(1 \mathrm{~atm}, 20^{\circ} \mathrm{C}\), and \(10 \mathrm{~m} / \mathrm{s}\). The total drag force acting on the upper surface of the plate is measured to be \(2.4 \mathrm{~N}\). Using the momentum-heat transfer analogy, determine the average convection heat transfer coefficient and the rate of heat transfer between the upper surface of the plate and the air. Evaluate the air properties at \(50^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).

A \(15-\mathrm{cm} \times 20\)-cm circuit board is being cooled by forced convection of air at \(1 \mathrm{~atm}\). The heat from the circuit board is estimated to be \(1000 \mathrm{~W} / \mathrm{m}^{2}\). If the airstream velocity is \(3 \mathrm{~m} / \mathrm{s}\) and the shear stress of the circuit board surface is \(0.075 \mathrm{~N} / \mathrm{m}^{2}\), determine the temperature difference between the circuit board surface temperature and the airstream temperature. Evaluate the air properties at \(40^{\circ} \mathrm{C}\) and $1 \mathrm{~atm}$.

Evaluate the Prandtl number from the following data: $c_{p}=0.5 \mathrm{Btu} / \mathrm{lbm} \cdot \mathrm{R}, k=2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot \mathrm{R}, \mu=0.3 \mathrm{lbm} / \mathrm{ft} \cdot \mathrm{s}$.

Air flows over a flat plate at $40 \mathrm{~m} / \mathrm{s}, 25^{\circ} \mathrm{C}\(, and \)1 \mathrm{~atm}\( pressure. \)(a)$ What plate length should be used to achieve a Reynolds number of \(1 \times 10^{8}\) at the end of the plate? (b) If the critical Reynolds number is \(5 \times 10^{5}\), at what distance from the leading edge of the plate would transition occur?

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