This document summarizes a numerical investigation of flow through an axisymmetric boat tail nozzle at transonic conditions using computational fluid dynamics (CFD). The study analyzed the effects of friction on adiabatic flow and determined a friction factor of 0.001452. CFD simulations using GAMBIT and FLUENT were conducted with a k-epsilon turbulence model to analyze pressure distributions, velocity vectors, and coefficient of pressure plots. Validation against experimental data showed reasonable agreement. The study concluded that CFD can predict nozzle aerodynamics, though turbulence models under predict pressures. Friction was found to impact real flows compared to isentropic assumptions. Future work could analyze shockwaves at Mach 0.8.