摘要
本文将试验,计算与外场实测相结合,论证了歼六飞机前起落架损伤折断的主要原因是前轮摆振,采取简单、合理、易行的措施,解决歼六飞机前起落架防摆抗断问题,取得显著效果。
By considering the results from experiments and calculations, it has been proved that the main reason of damage of nose landing gear of an aircraft is due to shimmy. By using an easy, simple and reasonable method, the anti-shimmy and break-proof problem of nose landing gear has been solved and a satisfying result has been obtained.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1989年第10期B495-B500,共6页
Acta Aeronautica et Astronautica Sinica
关键词
起落架
摆振
阻尼
应力
飞机
laoding gear, shimmy, damping, strees.
