Aircraft landing gear with electromagnetic damper

The article describes the design and computation of the aircraft landing gear with an electromagnetic-gas shock absorber. A numerical simulation of the landing impact was carried out at different values of the initial vertical velocity. The dependence of the optimal electric current in the winding o...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2021-01, Vol.1019 (1), p.12069
Hauptverfasser:	Zagidulin, A R, Podruzhin, E G
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft landing Electromagnets Landing gear Shock absorbers
Online-Zugang:	Volltext
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