前轮摆振适航审查时Moreland轮胎模型中τ的取值  

The Value τ of Moreland Model in Airworthiness Examination of Front Wheel Shimmy

作　　者：王杰[1] 顾宏斌[1] 陈大伟[1] 马千里[1] 

机构地区：[1]南京航空航天大学,江苏南京211106

出　　处：《现代工业经济和信息化》2017年第3期54-56,共3页Modern Industrial Economy and Informationization

摘　　要：针对摆振适航审查的需要,建立前轮摆振的数学模型和Moreland轮胎模型,并对此模型进行仿真来分析摆振现象,获得深入的认识,从而为适航审定提供要点线索和方法。As to the needs of airworthiness examination of shimmy, mathematical model and Moreland model of front wheel shimmy are built, and simulation of these models are analyzed and get in-depth understanding so as to provide key clues and methods of airworthiness certification.

关 键 词：适航 前轮摆振 Moreland轮胎模型 

分 类 号：U461.61[机械工程—车辆工程]