In a reversible adiabatic process the ration \(\left( {\frac{{{T_1}}}{{{T_2}}}} \right)\) is equal to:
A reversible adiabatic process is a thermodynamic process in which no heat is transferred into or out of the system (\(\Delta Q = 0\)), and the process is reversible, meaning it can be reversed without any change in the surroundings. For an ideal gas undergoing a reversible adiabatic process, the relationship between pressure (\(P\)) and volume (\(V\)) is given by:
\[PV^\gamma = \text{constant}\]
where \(\gamma\) is the adiabatic index, defined as the ratio of the specific heat at constant pressure (\(C_p\)) to the specific heat at constant volume (\(C_v\)), i.e., \(\gamma = C_p / C_v\).
We need to find the ratio of initial temperature (\(T_1\)) to final temperature (\(T_2\)). We can use the ideal gas law, which states:
\[PV = nRT\]
where \(n\) is the number of moles and \(R\) is the ideal gas constant. From this equation, we can express pressure \(P\) as \(P = \frac{nRT}{V}\) or volume \(V\) as \(V = \frac{nRT}{P}\).
Let's substitute the expression for \(P\) from the ideal gas law into the adiabatic process equation \(PV^\gamma = \text{constant}\):
\[\left(\frac{nRT}{V}\right)V^\gamma = \text{constant}\]
\[nRT V^{\gamma-1} = \text{constant}\]
Since \(nR\) is a constant, we get a relationship between temperature and volume:
\[TV^{\gamma-1} = \text{constant}\]
For two states (initial state 1 and final state 2) in the reversible adiabatic process, we have:
\[T_1 V_1^{\gamma-1} = T_2 V_2^{\gamma-1}\]
Rearranging this to find the ratio \(\frac{{{T_1}}}{{{T_2}}}}\):
\[\frac{{{T_1}}}{{{T_2}}}} = \frac{{{V_2^{\gamma-1}}}}{{{V_1^{\gamma-1}}}}} = \left(\frac{{{V_2}}}{{{V_1}}}}\right)^{\gamma-1}\]
Using \(v\) for volume as in the options, this is \(\left(\frac{{{v_2}}}{{{v_1}}}}\right)^{\gamma-1}\). This expression is equivalent to \(\left(\frac{{{v_1}}}{{{v_2}}}}\right)^{-(\gamma-1)}\), which is not in the given options in a matching form.
Now, let's substitute the expression for \(V\) from the ideal gas law into the adiabatic process equation \(PV^\gamma = \text{constant}\):
\[P\left(\frac{nRT}{P}\right)^\gamma = \text{constant}\]
\[P \left(\frac{(nR)^\gamma T^\gamma}{P^\gamma}\right) = \text{constant}\]
\[\frac{(nR)^\gamma T^\gamma}{P^{\gamma-1}} = \text{constant}\]
Since \((nR)^\gamma\) is a constant, we get a relationship between temperature and pressure:
\[\frac{{{T^\gamma}}}{{{P^{\gamma-1}}}}} = \text{constant}\]
For two states in the reversible adiabatic process:
\[\frac{{{T_1^\gamma}}}{{{P_1^{\gamma-1}}}}} = \frac{{{T_2^\gamma}}}{{{P_2^{\gamma-1}}}}}\]
Rearranging this to find the ratio \(\frac{{{T_1}}}{{{T_2}}}}\):
\[\frac{{{T_1^\gamma}}}{{{T_2^\gamma}}}} = \frac{{{P_1^{\gamma-1}}}}{{{P_2^{\gamma-1}}}}}\]
\[\left(\frac{{{T_1}}}{{{T_2}}}}\right)^\gamma = \left(\frac{{{P_1}}}{{{P_2}}}}\right)^{\gamma-1}\]
Taking the \(\gamma\)-th root of both sides:
\[\frac{{{T_1}}}{{{T_2}}}} = \left[\left(\frac{{{P_1}}}{{{P_2}}}}\right)^{\gamma-1}\right]^{1/\gamma} = \left(\frac{{{P_1}}}{{{P_2}}}}\right)^{\frac{{\gamma - 1}}{\gamma }}\]
Using \(p\) for pressure as in the options, this is \(\left(\frac{{{p_1}}}{{{p_2}}}}\right)^{\frac{{\gamma - 1}}{\gamma }}\).
Let's compare our derived formulas with the given options:
The derived formula for the temperature ratio in terms of pressure is \(\frac{{{T_1}}}{{{T_2}}}} = \left(\frac{{{p_1}}}{{{p_2}}}}\right)^{\frac{{\gamma - 1}}{\gamma }}\).
Therefore, the correct expression for the ratio \(\left( {\frac{{{T_1}}}{{{T_2}}}} \right)\) in a reversible adiabatic process is \(\left( {\frac{{{p_1}}}{{{p_2}}}} \right)^{\frac{{\gamma - 1}}{\gamma }}\).
Heat transfer in a cyclic process are +20 kJ, -5 kJ, -10 kJ and +15kJ. Net work done for this cycle will be given by:
An open system is one in which ______.
A system will be in thermodynamic equilibrium only if it is in ____.
A. Thermal equilibrium
B. Mechanical equilibrium
C. Chemical equilibrium
The gas constant (R) is equal to the _____ of two specific heats.
A series of operations, which takes place in a certain order and restore the initial conditions at the end, is known as