Advanced Search
Volume 27 Issue 3
Mar.  2001
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(3): 332-335.
WU Cun-hao, YANG Jia-ling, ZANG Shu-guang, et al. Study of Bird Impact Loading Model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 332-335. (in Chinese)
Citation: WU Cun-hao, YANG Jia-ling, ZANG Shu-guang, et al. Study of Bird Impact Loading Model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 332-335. (in Chinese)
shu

Study of Bird Impact Loading Model

  • 1.

    Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • 2. China Building Materials Academy

  • Received Date: 25 Sep 2000
  • Publish Date: 31 Mar 2001
    Abstract
  • To study the bird impact problem, one key point is to establish the bird impact loading model. This paper, based on the full scale bird impact tests, and detailed analysis the results of high-speed photography, dynamic strain gauge, puts forward that triangle pulse simply model could be simplified by bird impact loading of inclined impact process .The analysis results that calculate the simply model using finite element analysis tools are accordance with the results from full-scale bird impact tests.

     

    • FullText(HTML)
  • loading
    • References(1)
  • [1] GJB-2464-95,中华人民共和国国家军用标准[S]. [2] ASTM F330-79,宇航透明件的鸟撞试验方法[S]. [3] McCarty R E, Hart J L. Validation of the MAGNA computer program for nonlinear finite element analysis of aircraft transparency bird impact . AFWAL-TR-83-4154,1983. [4] Robert A. MAGNA:A finite element system for three-dimensional nonlinear static and dynamic structural analysis[J]. Computer & Structure,1981,(13):415~423. [5] Samuelson L A, Nisson F. Theoretical evaluation of the structure performance of Swedish fighter aircraft windshield subjected to impact . AD-P 003-235,1983. [6] McCarty R E. MAGNA computer simulation of bird impact on the TF-15 aircraft canopy . ADA140701, 1983. [7] Barber J P, Boehman L I. The modeling of bird impact loads . ADA065049,1978. [8] Wilbeck J S. Impact behavior of low strength projectiles . AFML-TR-77-134,1977.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2567) PDF downloads(910) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return