Landing Performance Study for Four Wheels Twin Tandem Landing Gear Based on Drop Test

The drop tests of a twin tandem landing gear with different filling parameters are carried out in two different landing attitudes (level and tail-down). The overload coefficient and power absorption efficiency are obtained. Curves of dynamic oscillation and pressure change for the pitch damper are o...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Wei Fang, Lingang Zhu, Youshan Wang
Format:	Article
Language:	English
Published:	MDPI AG 2022-06-01
Subjects:	drop test twin tandem landing gear landing impact pitch damper overload coefficients buffer system efficiency
Online Access:	https://www.mdpi.com/2226-4310/9/7/334