Author:
Alpatskiy Nikita,Pavlenko Alexander,Melnik Elizaveta,Kaprilevskaya Valeria,Zanin Boris
Abstract
The study was carried out on a model of a small-sized aircraft of the type of a flying wing, which has a V-shape in plan. The structure of the flow on the wing surface was studied depending on the angle of attack and deflection of the controls. Experiments were carried out to study the influence of the work of the distributed electric propulsion on the flow structure on the wing surface. As a result, flow patterns were obtained using the “soot-oil” visualization method for each flow regime.
Reference4 articles.
1. Marcus E. A., de Vries R., Raju Kulkarni A., Veldhuis L. L., Aerodynamic investigation of an over- the-wing propeller for distributed propulsion, in Proceedings of the 2018 AIAA Aerospace Sciences Meeting, 8-12 January 2018, Kissimmee, FL, USA (2018)
2. Kim H. D., Distributed propulsion vehicles, in Proceedings of the 27th Congress of the International Council of the Aeronautical Sciences, ICAS 2010, 7-13 March 2010, Cancun, Mexico (2010)
3. Investigation of the influence of controls on the flow around the UAV model
4. de Vries R., Vos R., Aerodynamic performance benefits of over-the-wing distributed propulsion for hybrid-electric transport aircraft, in Proceedings of the AIAA SCITECH 2022 Forum, 3-7 January 2022, San Diego, CA, USA, (2022)