Aeroelastic Response of Spinning Projectiles with Large Slenderness Ratio at Supersonic Speed

Obvious aeroelastic deformation occurs in spinning projectiles with large slenderness ratio, which seriously affects flight stability and maneuverability. This paper investigates the aeroelastic response of spinning projectiles with large slenderness ratio under supersonic speed. Based on a dynamic...

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Váldodahkkit:	Qi Liu, Juanmian Lei, Yong Yu, Jintao Yin
Materiálatiipa:	Artigo
Giella:	Inglês
Almmustuhtton:	MDPI AG 2023-07-01
Ráidu:	Aerospace
Fáttát:	spinning projectiles aeroelasticity dynamic response fluid–solid coupling numerical simulation
Liŋkkat:	https://www.mdpi.com/2226-4310/10/7/646
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