At DLR in Berlin, a series of experiments was performed on a laboratory scale fan rig to explore the potential of trailing edge blowing (TEB) for the attenuation of tonal noise of an axial fan stage. The model fan consisted of 18 blades, each of which was equipped with five internal flow channels, commonly provided with pressurized air through the rotor hub. In configuration 1, all five channels were utilized for noise control. In configuration 2, the outmost two internal channels were blocked by means of aluminum tape. The latter case provided substantial tonal noise reduction, whereas the former led to no acoustic impact. In order to reproduce the experimental result, an analytical acoustic model based on the flow field measured by the hot wires was utilized. The model considers the interaction of the rotor wakes with the stator and substitutes the real sources by a spatial distribution of dipoles on the blades. Thus, the impact of the trailing edge blowing is modelled via the wake velocity perturbations and the unsteady lift they induce on the stator blades. The predicted noise reductions achieved by the TEB approach are in fairly good agreement with the experiments. Moreover, the model provides helpful indications about the reason for the failure of conf. 1 to provide a noise reduction and the success of conf. 2 to do so.