An ideal gas flows isentropically through a convergingdiverging nozzle. At a section in the converging portion of the nozzle, \(A_{1}=0.1 \mathrm{~m}^{2}, p_{1}=600 \mathrm{kPa}(\) abs \(), T_{1}=20^{\circ} \mathrm{C}\), and \(\mathrm{Ma}_{1}=0.6\). For section (2) in the diverging part of the nozzle, determine \(A_{2}, p_{2}\), and \(T_{2}\) if \(\mathrm{Ma}_{2}=3.0\) and the gas is air.