Analytical Investigation of Aircraft Nosewheel Deflection Limit According to the Taxiing Speed

The rollover can be encountered due to excessive deflection of the nosewheel during takeoff and landing stages of the aircraft, so the nose-wheel deflection should be reasonably limited according to the taxiing speed.Based on the principle of the rollover phenomenon, the resultant moment of the airc...

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Bibliographic Details
Main Author: TANG Ruilin
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2021-06-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2020137?st=article_issue

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