CREATION OF AN EXPERIMENTAL CONTROL BODY (ELEVON) IN THE «FLYING WING» AERODYNAMIC SCHEME
Autor: | D. V. Elenin |
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Rok vydání: | 2021 |
Předmět: | |
Zdroj: | System analysis and logistics. 2:26-32 |
ISSN: | 2077-5687 |
DOI: | 10.31799/2077-5687-2021-2-26-32 |
Popis: | The article discusses the possibility of creating two schemes of an experimental control body in flight for a UAV of the "Flying Wing" scheme. The concept of creating a real prototype for an experiment in the Solidworks Flow environment and in a wind tunnel with a low incoming flow velocity is presented. Key words: wing, aerodynamic design, UAV, flying wing. |
Databáze: | OpenAIRE |
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