航空学报 > 2004, Vol. 25 Issue (4): 372-375

GARTEUR有限元模型修正与确认研究

费庆国, 张令弥, 郭勤涛   

  1. 南京航空航天大学振动工程研究所 江苏南京 210016
  • 收稿日期:2003-07-07 修回日期:2004-03-25 出版日期:2004-08-25 发布日期:2004-08-25

Case Study of FE Model Updating and Validation via an Aircraft Model Structure

FEI Qing-guo, ZHANG Ling-mi, GUO Qin-tao   

  1. Institute of Vibration Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2003-07-07 Revised:2004-03-25 Online:2004-08-25 Published:2004-08-25

摘要: 待修正参数的选择以及修正后模型的质量评估是有限元模型修正的两个重要问题。以欧洲学术界广泛采用的GARTEUR飞机模型为例,利用基于灵敏度分析的模型修正方法,通过仿真算例研究参数选择对模型修正质量的影响,并以试验数据为目标值对有限元模型进行修正与确认。为全面评估模型的修正质量,引入三级标准对修正后有限元模型进行确认。

关键词: 固体力学, 模型确认, 有限元法, 模型修正, 参数选择

Abstract: Parameter selection and quality validation are of great importance in finite element model updating. This paper presents some results which demonstrate the relationship between parameter selection and updated model's quality through simulation cases. Three quality levels with corresponding validation criteria are employed with an emphasis on updated model's prediction ability. Results of updating based on experimental modal test data are shown as an application example. An aircraft test structure, GARTEUR, which is generally utilized in Europe, is employed in both the simulation case and the experimental case. Sensitivity-based model updating approach is applied.

Key words: solid mechanics, model validation, finite element method, model updating, parameter selection