An investigation of an active landing gear system to reduce aircraft vibrations caused by landing impacts and runway excitations-Reference-Cited by-同舟云学术

An investigation of an active landing gear system to reduce aircraft vibrations caused by landing impacts and runway excitations

Published:2008-10 Issue:1-2 Volume:317 Page:50-66
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Wang Haitao,Xing J.T.,Price W.G.,Li Weiji

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference30 articles.

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3. An experimental–analytical routine for the dynamic qualification of aircraft operating on rough runway surfaces;Freymann;AGARD R-731,1987

4. T. Catt, D. Cowling, A. Shepherd, Active landing gear control for improved ride quality during ground roll, SDL Report No. 232, Stirling Dynamics Limited, 1992.

5. Dynamic response of landing gears on rough repaired runway;Lee;Menasco Aero Systems Division,1998

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