This research aims to characterise the aerodynamic flow around a container freight train and investigate how changing the container loading configuration affects the magnitude of aerodynamic forces measured on a container. Experiments were carried out using a 1/25th scale moving model freight train at the University of Birmingham's TRAIN rig facility. The model was designed to enable different container loading configurations and train lengths to be tested. A series of experiments to measure slipstream velocities and static pressure were undertaken to assess the influence of container loading configuration. Experiments to measure aerodynamic loads on a container were carried out using an on-board pressure monitoring system built into a specifically designed measuring container. A collation of full scale freight data from previous studies provided a tool to validate model scale data.Analysis of freight data found it was possible to present slipstream results as a series of flow regions. Clear differences in slipstream development and aerodynamic load coefficients were observed for differing container loading configurations. Velocity and pressure magnitudes measured in the nose region were larger than values observed previously. For container loading efficiencies higher than 50% boundary layer growth stabilises rapidly, however, for less than 50% continual boundary layer growth was observed until after 100m when stabilisation occurs. Velocities in the lateral and vertical directions have magnitudes larger than previously observed; increasing the overall magnitude by ∼10%. Comparison of model and full scale data showed good agreement, indicating Reynolds number independence. An analysis of TSI safety limits found results lie close to, but do not break, existing limits. Aerodynamic load coefficients were compared with previous studies and shown to be characteristic of typical values measured for a 30• yaw angle; however, differences between static wind tunnel and moving model results were discovered.