An Aerodynamic Design Method to Improve the High-Speed Performance of a Low-Aspect-Ratio Tailless Aircraft

An Aerodynamic Design Method to Improve the High-Speed Performance of a Low-Aspect-Ratio Tailless Aircraft

This paper puts forward an aerodynamic design method to improve the high-speed aerodynamic performance of an aircraft with low-aspect-ratio tailless configuration. The method can ameliorate the longitudinal moment characteristics of the configuration by designing and collocating the key section airf...

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Bibliographic Details
Main Authors: Zhongyuan Liu, Lie Luo, Binqian Zhang
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Applied Sciences
Subjects:
aerodynamic design
low-aspect-ratio tailless configuration
pitching moment
Online Access:https://www.mdpi.com/2076-3417/11/4/1555

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