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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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Hlavní autoři: Cong Xie, Guoquan Tao, Zhe Wu
Médium: Artigo
Jazyk:Inglês
Vydáno: MDPI AG 2021-05-01
Edice:Applied Sciences
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On-line přístup:https://www.mdpi.com/2076-3417/11/10/4698
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