Step 1: Understanding the Question:
This problem involves calculating steady-state, one-dimensional heat conduction through a plane wall with known dimensions, thermal conductivity, and boundary temperatures.
Step 2: Key Formula or Approach:
Fourier's Law of Heat Conduction for a plane wall is expressed as:
\[ Q = \frac{k A \Delta T}{L} \]
Where:
$Q$ is the rate of heat transfer (W).
$k$ is the thermal conductivity of the wall ($\text{W/m}\cdot\text{K}$).
$A$ is the heat transfer area ($\text{m}^2$).
$\Delta T$ is the temperature difference across the wall (K or $^\circ\text{C}$).
$L$ is the thickness of the wall (m).
Step 3: Detailed Explanation:
• Let's list the given parameters:
Thickness, $L = 0.1\text{ m}$
Thermal conductivity, $k = 50\text{ W/m}\cdot\text{K}$
Surface area, $A = 2\text{ m}^2$
Temperature difference, $\Delta T = 100\text{ K}$
• Substitute these values into Fourier's Law:
\[ Q = \frac{50 \times 2 \times 100}{0.1} \]
• Simplify the numerator:
\[ 50 \times 2 \times 100 = 10,000\text{ W} \]
• Divide by the wall thickness:
\[ Q = \frac{10,000}{0.1} = 100,000\text{ W} \]
• Convert the heat transfer rate into kilowatts ($\text{kW}$):
\[ Q = \frac{100,000}{1,000}\text{ kW} = 100\text{ kW} \]
Step 4: Final Answer:
The rate of heat transfer through the plane wall is $100\text{ kW}$, which corresponds to option (B).