The paper presents results of the unmanned aerial vehicle wing shape optimization, developed at Tomsk State University [1] (Ismailov K.K. et. al. Development of plane type UAV digital model // 19th International Conference “Aviation and Cosmonautics” (AviaSpace-2020), 23-27 November, 2020. Moskow. Abstracts. - Publishing house “Pero”, 2020. - 980 p. P. 59-60). The RANS equations were solved using SST k - Ю turbulence model within OpenFOAM. The wing shape was optimized using the method of gradients. According to the research results, a more stalling-stable wing a bit loosed aerodynamic efficiency was obtained.
Перспективы развития фундаментальных наук : сборник научных трудов XVIII Международной конференции студентов, аспирантов и молодых ученых, 27–30 апреля 2021 г.. Томск, 2021. Т. 3 : Математика. С. 37-39