Research on the Performance of Slender Aircraft with Flare-Stabilized-Skirt

In this paper, a morphing aircraft with a deployable flared skirt is proposed, and the influence of the flare skirt on the static stability of hypersonic aircraft is studied. The theoretical model of static stability of slender aircraft is established, and the position of the center of pressure can...

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Bibliographic Details
Main Authors: Xueting Pan, Honghao Yue, Shufeng Liu, Fei Yang, Yifan Lu, Gang Chen
Format: Article
Language:English
Published: MDPI AG 2023-09-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/10/844