Modeling of shimmy oscillations in aircraft landing gear

Publisher： Edp Sciences

E-ISSN： 2261-236x|133|issue|01007-01007

ISSN： 2261-236x

Source： MATEC Web of conference, Vol.133, Iss.issue, 2017-11, pp. : 01007-01007

Access to resources Favorite

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Fluid Similarity Criterions in Aircraft Landing Gear

By  

MATEC Web of conference, Vol. 151, Iss. issue, 2018-02 ,pp. : 04007-04007

Edp Sciences

Access to resources Recommend Favorite

Control of shimmy vibration in aircraft landing gears based on tensor product model transformation and twisting sliding mode algorithm

By  

MATEC Web of conference, Vol. 161, Iss. issue, 2018-04 ,pp. : 02001-02001

Edp Sciences

Access to resources Recommend Favorite

A New Method for Determining Horizontal Impact Load Based on Rotational Speed of Aircraft Wheel in Landing Gear Drop Test

By  

MATEC Web of conference, Vol. 114, Iss. issue, 2017-07 ,pp. : 03004-03004

Edp Sciences

Access to resources Recommend Favorite

The Review and Development of the Landing Gear Emergency Release System

By  

MATEC Web of conference, Vol. 114, Iss. issue, 2017-07 ,pp. : 03016-03016

Edp Sciences

Access to resources Recommend Favorite

Gear noise modeling

By Singh Rajendra   Kinzel Gary L.   Houser Donald R.  

INTER-NOISE and NOISE-CON Congress and Conference Proceedings, Vol. 1980, Iss. 3, 1980-12 ,pp. : 165-168

Institute of Noise Control Engineering

Access to resources Recommend Favorite