Virtual health monitoring system for wing structure

Fangyi Wan, Zeng Qin

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

Based on virtual simulation results, the structural health monitoring (SHM) system for the wing structure was established, which could detect the structural damages. With the FE model of the wing structure in the aerodynamic loads conditions, the response parameters of the wing can be calculated to reveal the damages characteristics. There are obvious differences between damaged wing and normal wing which can be utilized to detect the damages and locate the damaged positions.

源语言英语
主期刊名MEMS and Mechanics
534-539
页数6
DOI
出版状态已出版 - 2013
活动2013 International Conference on MEMS and Mechanics, MEMSM 2013 - Wuhan, 中国
期限: 15 3月 201316 3月 2013

出版系列

姓名Advanced Materials Research
705
ISSN(印刷版)1022-6680

会议

会议2013 International Conference on MEMS and Mechanics, MEMSM 2013
国家/地区中国
Wuhan
时期15/03/1316/03/13

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