航空学报 > 2004, Vol. 25 Issue (6): 577-580

飞机风挡鸟撞动响应分析方法研究

张志林, 姚卫星   

  1. 南京航空航天大学飞行器系 江苏南京 210016
  • 收稿日期:2003-11-12 修回日期:2004-06-30 出版日期:2004-12-25 发布日期:2004-12-25

Research on Dynamic Analysis of Bird Impact on Aircraft Windshield

ZHANG Zhi-lin, YAO Wei-xing   

  1. Department of Aircraft Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2003-11-12 Revised:2004-06-30 Online:2004-12-25 Published:2004-12-25

摘要: 建立了鸟体模型和风挡玻璃破坏准则,形成了一套完整的风挡鸟撞动响应分析方法。并对某型号风挡进行了鸟撞动响应分析,得出了鸟的运动轨迹和风挡的位移、应力、应变响应以及风挡玻璃的鸟撞临界速度,经与试验结果比较,两者吻合较好。

关键词: 风挡, 鸟撞, 耦合解法, 解耦解法, 临界速度

Abstract: A bird model which is used in bird-windshield strike analysis is established in comparison with to the standard solutions, and the failure criterion of windshield suggested is that the strain produced is greater than the critical strain of the windshield material. Then LS-DYNA is employed to analysis the bird-windshield impact response. The dynamic stress, strain and displacement of the windshield are obtained, and the critical velocity when the windshield failure is also gotten on the FE analysis. The analytical results are compared to those of the experiment and both are consistent fairly well.

Key words: windshield, bird impact, coupled solution, decoupled solution, critical velocity