Hot gas ingestion into turbine rim seal cavities is an important concern for engine designers. To prevent ingestion, rim seals use high pressure purge flow; however, the penalty is excessive use of purge flow decreases engine thermal efficiency. In this paper, a one-stage turbine operating at engine representative conditions was used to study the effect of steady and time-resolved under-platform cavity temperatures and pressures across a range of coolant flow rates in the presence of vane trailing edge (VTE) flow. This study correlates time-resolved pressure with time-resolved temperature to identify primary frequencies driving ingestion. At certain flow rates, time-resolved pressures are out of phase with temperatures, indicating ingestion. Measurements from high-frequency response pressure sensors in the rim seal and vane platform were used to determine rotational speed and quantity of large-scale structures (cells). A computational model using Unsteady Reynolds-averaged Navier-Stokes (URANS) was applied to determine swirl ratio in the rim seal cavity and time-resolved rim sealing effectiveness. Experimental results confirm at low purge flow rates, VTE flow influences the unsteady flow field by decreasing pressure unsteadiness in the rim seal cavity. Results show an increase in purge flow increases the number of unsteady cells and decreases their rotational speed. However, VTE flow was shown to not significantly change cell speed and count. Simulations point to the importance of the large-scale cell structures in influencing rim sealing unsteadiness, which is not captured in current rim sealing predictive models.