Investigation of aerodynamic performance of bladeless fan-based fluidic propulsion integrated on aircraft wing

Abstract Fluidic propulsion based on bladeless fan technology has shown strong potential to generate sufficient thrust for lightweight commuter aircraft. Bladeless fans work by entraining and directing ambient air, a feature that can be harnessed not only for thrust generation but also to augment lift. This research investigates the integration of bladeless fans over aircraft wings through both two-dimensional and three-dimensional computational simulations, supplemented by wind tunnel experiments. Multiple configurations were examined – varying fan height, spanwise and chordwise placement, orientation and the number of fan units – and compared against the aerodynamic performance of a baseline wing. The results demonstrate that leading-edge fan placement outperforms trailing-edge configurations, particularly in the post-stall regime. For 2D cases, a maximum of 71% lift increment in the post-stall region with 25% increase in the stall angle was observed. Additionally, the bladeless fans effectively reshape the flow field over the wing, increasing lift at the cost of higher drag relative to the baseline. For 2D cases, a 50% increase in zero lift drag was observed; however, 39% reduction was also observed in post-stall region. Among all configurations, the triple-bladeless-fanjet arrangement delivered the best performance, with further gains observed when a positive incidence angle was applied to the fans. An increase of 45% in lift coefficient was observed for triple fan configuration. These computational findings were validated through wind tunnel tests on a propeller-driven aircraft model, where the bladeless fan-equipped version exhibited superior aerodynamic performance compared to the baseline.