太原理工大学学报2018，Vol.49Issue(3)：488-493,6.DOI:10.16355/j.cnki.issn1007-9432tyut.2018.03.020
基于ADAMS的舰载机拦阻着舰仿真分析
Simulation Analysis of Carrier Aircraft Arresting Landing Based on ADAMS
摘要
Abstract
This paper established the aircraft arresting hook rigid-flexible coupling dynamics model,and in ADAMS dynamics simulation software,according to the experimental data ob-tained from a car with the same mass the quality of the car,a method of applying arresting loads was put forward to analyze the multi-body dynamics simulation of rigid-flexible coupling for carri-er-based UAV aircraft landing.The transmission path of aircraft fuselage overload and the distri-bution of the stress and strain of the fuselage during the arresting process were analyzed.The simulation results show that the simulation method can effectively simulate the landing process of the carrier-based aircraft under the coupling of complex and strong nonlinear loads,and provide a reference for the research of the carrier-based aircraft's arresting and landing process and the de-sign of the fuselage structure.关键词
舰载飞机/拦阻着舰/刚柔耦合动力学/动态响应Key words
carrier aircraft/arresting landing/rigid flexible coupled multibody dynamics/dy-namic response分类
航空航天引用本文复制引用
高华峰,张晓晴,李志强,张闰,李永刚,朱小龙..基于ADAMS的舰载机拦阻着舰仿真分析[J].太原理工大学学报,2018,49(3):488-493,6.基金项目
国家自然科学基金资助项目(11672110,11472110,11372113) （11672110,11472110,11372113）
