Three acceleration sensors are used to obtain the vibration data.Findings\nThe results show that the increase in the amplitude of the vibration is directly related to the decrease in lift. These findings indicate that this approach could be beneficial in detecting stall on airfoil-type structures....
Bari, A.A.; Mashud, M.; Ali, H. Role of partially bumpy surface to control the flow separation of an airfoil.ARPN J. Eng. Appl. Sci.2012,7, 584–587. [Google Scholar] Lang, A.; Habegger, M.L.; Motta, P. Shark skin drag reduction. InEncyclopedia of Nanotechnology; Springer: Do...
To focus on the anti-icing effect and aerodynamic performance of the airfoil, we assume a constant temperature at the heating area. The icing simulations of the HAARP-II and NACA0012 airfoils are numerically validated by comparing their results with the experimental data. For the NACA0012 airfoil...
A Wind Tunnel Experimental Study of Icing on NACA0012 Aircraft Airfoil with Silicon Compounds Modified Polyurethane Coatings. Materials. 2021; 14(19):5687. https://doi.org/10.3390/ma14195687 Chicago/Turabian Style Przybyszewski, Bartlomiej, Rafal Kozera, Zuzanna D. Krawczyk, Anna Boczkowska, ...