To resolve this problem, we must establish the relationship between pressure \(P\), temperature \(T\), and the specific heat ratio \(\gamma = \frac{C_p}{C_v}\) under adiabatic conditions. The problem states that the gas pressure is directly proportional to the cube of its absolute temperature, which can be represented as:
\(P \propto T^3\)
For an adiabatic process, the pressure-temperature relationship is defined as:
\(PT^{-\frac{\gamma}{\gamma - 1}} = \text{constant}\)
Given \(P \propto T^3\), we equate the exponents of \(T\):
\(T^3 \cdot T^{-\frac{\gamma}{\gamma - 1}} = \text{constant}\)
\(3 - \frac{\gamma}{\gamma - 1} = 0\)
Solving the equation yields:
\(3 = \frac{\gamma}{\gamma - 1}\)
\(3(\gamma - 1) = \gamma\)
\(3\gamma - 3 = \gamma\)
\(2\gamma = 3\)
\(\gamma = \frac{3}{2}\)
Thus, the specific heat ratio \(\frac{C_p}{C_v}\) is \(\gamma = \frac{3}{2}\).
The correct answer is:
\(\frac{3}{2}\)
Analysis of Options: