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Performance Prediction and Design of Stratospheric Propeller

In this paper, a performance prediction method is proposed for the design of a stratospheric propeller. The Spalart–Allmaras (S–A) model was used to calculate the airfoil performance of FX63, and the polynomial fitting method was utilized to establish the airfoil database of the lift and drag coeffi...

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Главные авторы: Cong Xie, Guoquan Tao, Zhe Wu
Формат: Artigo
Язык:Inglês
Опубликовано: MDPI AG 2021-05-01
Серии:Applied Sciences
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Online-ссылка:https://www.mdpi.com/2076-3417/11/10/4698
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