Abstract
Results of the aerodynamic coefficients imitation of wing airfoils and helicopter blades are presented. The modeling is carried out using the artificial neural network algorithms. The dependencies of the lift coefficient and the drag coefficient on the angle of attack are imitated for various airfoil geometries.
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 2, pp. 164 - 168.
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Girfanov, A.M., Ledyankina, O.A. & Romanova, E.V. Investigation of Imitational Modeling Applicability for Aerodynamic Coefficients of Airfoils (Blades). Russ. Aeronaut. 64, 355–359 (2021). https://doi.org/10.3103/S1068799821020252
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DOI: https://doi.org/10.3103/S1068799821020252