A vehicle's refueling system including components which make up the onboard refueling vapor recovery (ORVR) system must be designed to meet federally set evaporative hydrocarbon emission regulations and other performance issues inherent to the refueling process such as premature click-off and spit-back. A CFD model able to predict the performance of a vehicle's refueling system could be a valuable tool towards the development of future designs, saving the OEM's time and money in the R&D phases. To create an adequate model for the computer aided engineering of a modern refueling systems, it is paramount to accurately predict the fluid dynamics through and out of a gasoline refueling gun, as this is a key inlet condition of any refueling system. This study aims to validate CFD simulations which predict the fluid dynamics through a refueling gasoline pump nozzle. The commercial CFD software, Star-CCM+ was used to model gasoline flow through two gasoline nozzle geometries. The CFD domain for a Husky X1 and an OPW 11B were created using PTC Creo Parametric, by way of physical measurements taken of the deconstructed nozzles. Experiments conducted and compared to the CFD results. It was found that the OPW 11B produced a divergent spray whereas the Husky X1 delivered a narrow jet like fuel spray. It was found that modeling of the nozzle internal fluid dynamics through the air entrainment and shut-off port geometries were needed to accurately capture fuel spray behavior, as demonstrated by experiments. Mesh independence and time independence studies were conducted, as well as different inlet techniques to simulate air entrainment present in the nozzles due to their shut-off port function. The study acts as a guide for future simulations involving fuel filling necks and tanks, and serves to suggest mesh, time step and solver settings to achieve the highest quality simulation.