Air at 20 degree Celsius flows over a flat plate maintained at 75 degr...
Explanation: h = – k/ (t s – t infinity) [d t/d y] y = 0 and d t/d y = – 50 * 10 3 degree Celsius/m.
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Air at 20 degree Celsius flows over a flat plate maintained at 75 degr...
To estimate the value of the local heat transfer coefficient, we can use the Newton's Law of Cooling, which states that the rate of heat transfer between a solid surface and a fluid is directly proportional to the temperature difference between them. Mathematically, it can be expressed as:
q = h * A * ΔT
Where:
q is the rate of heat transfer
h is the local heat transfer coefficient
A is the surface area in contact with the fluid
ΔT is the temperature difference between the surface and the fluid
In this case, we have:
ΔT = 75°C - 50°C = 25°C
A = 1 m² (assuming the surface area is 1 m² for simplicity)
We need to convert the temperature difference to Kelvin scale for consistent units:
ΔT = 25°C + 273.15 = 298.15 K
Now, we can rearrange the equation to solve for h:
h = q / (A * ΔT)
The rate of heat transfer (q) can be calculated using Fourier's Law of Heat Conduction:
q = k * A * (dT / dx)
Where:
k is the thermal conductivity of air
A is the cross-sectional area perpendicular to the direction of heat transfer
dT/dx is the temperature gradient across the distance x
In this case, the distance x is given as 0.5 mm, which is equivalent to 0.0005 m. The temperature gradient (dT/dx) can be calculated as:
dT/dx = (50°C - 20°C) / 0.0005 m = 60,000 K/m
Substituting these values into Fourier's Law of Heat Conduction:
q = 0.0266 W/mK * 1 m² * 60,000 K/m = 1,596 W
Now, we can substitute the calculated value of q into the equation for h:
h = 1,596 W / (1 m² * 298.15 K) = 5.36 W/m²K
Therefore, the estimated value of the local heat transfer coefficient is 5.36 W/m²K. None of the given options match this value, so there might be an error in the question or the answer choices provided.