In this work, the method of S. K. Godunov has been implemented to define the ballistic characteristics of the nozzle and to solve the integral equations of the boundary layer in order to determine its parameters and friction losses. There was conducted testing and comparison of the calculation results of the developed program with the theoretical data of other authors.
Перспективы развития фундаментальных наук : сборник научных трудов XVII Международной конференции студентов, аспирантов и молодых ученых, Россия, Томск, 21-24 апреля 2020 г.. Томск, 2020. Т. 3 : Математика. С. 7-9