Improvement of characteristics of the ring input device of the aviation power plant with the screwfanter

The article considers the method of improving the characteristics of the ring inlet device, taking into account the influence of the propeller of an aircraft power plant with a turboprop engine. It is shown that increasing the total pressure loss in the inlet device by 5% increases, approximately, t...

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Auteurs principaux: Олег Володимирович Жорник, Ігор Федорович Кравченко, Михайло Михайлович Мітрахович
Format: article
Langue:EN
RU
UK
Publié: National Aerospace University «Kharkiv Aviation Institute» 2021
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Accès en ligne:https://doaj.org/article/417b15d927424c6f91b8729f6a0a3904
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