摘要
针对基于“静载荷”模型的飞机载荷标定技术现状,分析了静载荷模型的优缺点,探索了考虑惯性力、弹性力、阻尼力的“动载荷”标定模型的建立方法,对改进现有标定模型具有一定的参考意义。
Aiming at the current situation of aircraft load calibration technology based on“static load”model,the advantages and disadvantages of static load model are analyzed.The method of establishing calibration model of“dynamic load”considering inertia force,elastic force and damping force is explored.
作者
侯乔乔
Hou Qiaoqiao(Aircraft Strength Research Institute of China,Xi'an Shaanxi 710065,China)
出处
《工程与试验》
2019年第2期44-45,共2页
Engineering and Test
关键词
动载荷
惯性力
弹性力
阻尼力
dynamic load
inertia force
elastic force
damping force
