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В данной работе представлен метод параметрической оптимизации, с помощью которого была найдена оптимальна форма фюзеляжа самолета-амфибия. В программном пакете ANSYS получены основные аэродинамические характеристики. В модельной задаче создана параметрическая модель профиля крыла.
In this research, we present a method of parametric optimization, with the use of which the optimal shape of the fuselage of the amphibian aircraft was found. In the software ANSYS basic aerodynamic characteristics were obtained. In the model problem, a parametric model of the wing profile was created.
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