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https://dx.doi.org/10.18720/sp...

Other literature type . 2018

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descriptionPublicationkeyboard_double_arrow_right Other literature type 01 Jan 2018 Russian Publisher:Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾

doi: 10.18720/spbpu/3/2018/vr/vr18-51

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Abstract

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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