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

Publisher: Edp Sciences

E-ISSN: 2261-236x|114|issue|03004-03004

ISSN: 2261-236x

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

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Abstract