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...
Main Author: | |
---|---|
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 |