Affiliation:
1. University of Nottingham
2. Beijing Institute of Technology
Abstract
Abstract
A joint study utilising experimental and numerical methods was carried out to investigate the aerodynamic effect of a rudder-mounted slat on a vertical stabiliser. The wind tunnel test results showed that the side force coefficient was increased by up to 4% while the drag coefficient was unchanged when the rudder deflection angle was set to δ = 30°. Large eddy simulation (LES) results suggested that the rudder-mounted slap can increase the circulation around the vertical stabiliser, showing that the flow from the upstream recirculating regions was drawn towards the rudder surface. Associated changes in the turbulent flow field, including the mean and turbulent flow field and the vortical structure are also presented to understand the flow control mechanism by the rudder-mounted slat.
Publisher
Research Square Platform LLC
Reference48 articles.
1. Arra, A., Anekar, N., Nimbalkar, S.: Aerodynamic effects of leading edge (LE) slats and slotted trailing edge (TE) flaps on NACA-2412 aerofoil in prospect of optimization. Materials Today: Proceedings. 44 587–595 (2021)
2. Aerofoil–slat arrangement model design for wind turbines in fuzzy environment;Atalay KD;Neural Comput. Appl.,2020
3. Effect of flap and slat riggings on 2-D high-lift aerodynamics;Balaji R;J. Aircr.,2006
4. Numerical analysis of aerodynamic performance of rotors with leading edge slats;Bangalore A;Comput. Mech.,1996
5. Assessment of leading-edge devices for stall delay on an aerofoil with active circulation control;Burnazzi M;CEAS Aeronaut. J.,2014