A New Design Model of an MR Shock Absorber for Aircraft Landing Gear Systems Considering Major and Minor Pressure Losses: Experimental Validation

This work presents a novel design model of a magnetorheological (MR) fluid-based shock absorber (MR shock absorber in short) that can be applied to an aircraft landing gear system. When an external force acts on an MR shock absorber, pressure loss occurs at the flow path while resisting the fluid fl...

Ausführliche Beschreibung

Bibliografische Detailangaben

Hauptverfasser:	Byung-Hyuk Kang, Jai-Hyuk Hwang, Seung-Bok Choi
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	MDPI AG 2021-08-01
Schriftenreihe:	Applied Sciences
Schlagworte:	magnetorheological (MR) fluid MR shock absorber aircraft landing gear valve path major and minor pressure losses impact energy
Online-Zugang:	https://www.mdpi.com/2076-3417/11/17/7895
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