Concept:
When a bar of length $L$ with a thermal expansion coefficient $\alpha$ undergoes a temperature change $\Delta T$, its free thermal expansion change in length is $\delta_{\text{th}} = \alpha L \Delta T$. If this expansion is completely prevented by rigid boundary supports, a compressive thermal strain develops in the bar:
\[
\epsilon = \frac{\delta_{\text{th}}}{L} = \alpha \Delta T
\]
According to Hooke's Law, the resulting internal thermal stress $\sigma$ depends on the Young's Modulus $E$ of the material:
\[
\sigma = E \epsilon = \alpha E \Delta T
\]
Step 1: Extracting the proportional relations from the problem statement.
Let us list the material property relationships given for Bar A and Bar B:
• Coefficient of thermal expansion: $\alpha_B = 2\alpha_A$
• Young's Modulus: $E_B = 2E_A$
• Both bars undergo the exact same temperature increase: $\Delta T_A = \Delta T_B = \Delta T$
Step 2: Writing down the stress equations for each bar.
Using the thermal stress formula for Bar A:
\[
\sigma_A = \alpha_A E_A \Delta T
\]
Using the thermal stress formula for Bar B, and substituting its properties in terms of Bar A:
\[
\sigma_B = \alpha_B E_B \Delta T = (2\alpha_A)(2E_A)\Delta T = 4 \alpha_A E_A \Delta T
\]
Step 3: Finding the ratio between the stresses.
Comparing the two stress equations shows that the stress developed in Bar B is four times larger than the stress in Bar A:
\[
\sigma_B = 4\sigma_A \quad \Rightarrow \quad \frac{\sigma_B}{\sigma_A} = 4
\]
The ratio between the stresses in the two bars is exactly $4$, which corresponds to Option (C).