Figure 2 shows the geometry of a typical saw-tooth serration, where 2h is the serration height (or amplitude), λ is the width, and Ɵ is the inclined angle. According to Howe10, in order to use the saw-tooth serration at the propeller trailing edge to reduce noise, some important geometry parameters need to be considered. The ratio between half height of the serration and the boundary layer thickness at trailing edge (h/δ) should larger than 0.25, otherwise the amplitude of the serration would be too small, and the turbulent eddies would pass over the saw-tooth without significant interaction. Thus, the system will experience no noise reduction. Secondly, the inclined angle should smaller than 45 degrees, which means the width/height ratio (λ/h) of the serration will smaller than 4.