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Acta Mechanica Solida Sinica

, Volume 32, Issue 1, pp 40–49 | Cite as

An Experimental and Numerical Study of Bird Strike on a 2024 Aluminum Double Plate

  • Jun LiuEmail author
  • Zongxing Liu
  • Naidan Hou
Article
  • 34 Downloads

Abstract

This paper presents an experimental and numerical study of the bird strike on a 2024-T3 aluminum double plate. The experiments are carried out at a desired impact velocity of 150 m/s. The explicit finite element software PAM-CRASH is used to simulate the bird-strike experiments, and a coupled SPH-FE method is adopted, where the bird is modeled using the SPH method with the Murnaghan EOS and the structure is meshed with finite elements. The material parameters are identified by an optimization process, and the simulated dynamic responses of bird strike are compared with experimental measurements to verify the numerical model. The displacement and strain of the plate as well as the final deformation and damage show good agreement between the simulation and the experimental results. It suggests that the coupled SPH-FE method can provide an effective tool in designing bird-strike-resistant aircraft component.

Keywords

Bird strike Experiment Simulation SPH PAM-CRASH 

Notes

Acknowledgements

This work was supported by the National Natural Science Foundation of China (Nos. 11472225 and 11102168).

References

  1. 1.
    Georgiadis S, Gunnion AJ, Thomson RS, Cartwright BK. Bird-strike simulation for certification of Boeing 787 composite moveable trailing edge. Compos Struct. 2008;86:258–68.CrossRefGoogle Scholar
  2. 2.
    Heimbs S. Computational methods for bird strike simulations: a review. Comput Struct. 2011;89(23–24):2093–112.CrossRefGoogle Scholar
  3. 3.
    Mao RH, Meguid SA, Ng TY. Finite element modeling of a bird striking an engine fan blade. J Aircraft. 2007;44(2):583–96.CrossRefGoogle Scholar
  4. 4.
    Meguid SA, Mao RH, Ng TY. FE analysis of geometry effects of an artificial bird striking an aeroengine fan blade. Int J Impact Eng. 2008;35(6):487–98.CrossRefGoogle Scholar
  5. 5.
    Jenq ST, Hsiao FB, Lin IC, Zimcik DG, Ensan MN. Simulation of a rigid plate hit by a cylindrical hemi-spherical tip-ended soft impactor. Comput Mater Sci. 2007;39:518–26.CrossRefGoogle Scholar
  6. 6.
    Mao RH, Meguid SA, Ng TY. Transient three dimensional finite element analysis of a bird striking a fan blade. Int J Mech Mater Des. 2008;4:79–96.CrossRefGoogle Scholar
  7. 7.
    Wang FS, Yue ZF. Numerical simulation of damage and failure in aircraft windshield structure against bird strike. Mater Des. 2010;31(2):687–95.CrossRefGoogle Scholar
  8. 8.
    Audic S, Berthillier M, Bonini J, Bung H, Combescur A. Prediction of bird impact in hollow fan blades. In: The \(36^{th}\)AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Huntsvile, Alabama, 16–19 July (2000).Google Scholar
  9. 9.
    McCarty MA, Xiao JR, McCarthy CT, Kamoulakos A, Ramos J, Gallard JP, Melito V. Modeling of bird strike on an aircraft wing leading edge made from fiber metal laminate—part 2: modeling of impact with SPH bird model. Appl Compos Mater. 2004;11:317–40.CrossRefGoogle Scholar
  10. 10.
    Liu J, Li Y, Gao X. Bird strike on a flat plate: experiments and numerical simulations. Int J Impact Eng. 2014;70:21–37.CrossRefGoogle Scholar
  11. 11.
    PAM-CRASH-2006 Solver Reference Manual (Version 3.0), engineering systems international, 20 Rue Saarinen, Silic 270, 94578 Rungis-Cedex, France (2006).Google Scholar
  12. 12.
    Goyal VK, Huertas CA, Vasko TJ. Bird-strike modeling based on the Lagrangian formulation using LS-DYNA. Am Trans Eng Appl Sci. 2013;2(2):57–81.Google Scholar
  13. 13.
    Goyal VK, Huertas CA, Vasko TJ. Smooth particle hydrodynamic approach for bird-strike analysis using LS-DYNA. Am Trans Eng Appl Sci. 2013;2(2):83–107.Google Scholar
  14. 14.
    Goyal VK, Huertas CA, Vasko TJ. Arbitrary Lagrange Eulerian approach for bird-strike analysis using LS-DYNA. Am Trans Eng Appl Sci. 2013;2(2):109–32.Google Scholar
  15. 15.
    Johnson AF, Holzapfel M. Modeling soft body impact on composite structures. Compos Struct. 2003;61:103–13.CrossRefGoogle Scholar
  16. 16.
    Barber JP, Taylor HR, Wilbeck JS. Bird impact force and pressures on rigid and compliant targets. Technical report AFFDL-TR-77-60. Air Force Flight Dynamics Laboratory, May 1978.Google Scholar
  17. 17.
    Liu MB, Liu GR. Restoring particle consistency in smoothed particle hydrodynamics. Appl Numer Math. 2006;56(1):19–36.MathSciNetCrossRefzbMATHGoogle Scholar
  18. 18.
    Vignjevic R, Reveles J, Lukyanof A. Analysis of compressor blade behaviour under bird impact. In: International conference on computational methods for coupled problems in science and engineering; 2005. p.1–14.Google Scholar
  19. 19.
    Liu J, Li Y, Shi X. Parameters inversion on bird constitutive model, part 2: study on model parameters inversion. Acta Aeronaut Astronaut Sin. 2011;32(5):812–21.Google Scholar

Copyright information

© The Chinese Society of Theoretical and Applied Mechanics 2018

Authors and Affiliations

  1. 1.School of AeronauticsNorthwestern Polytechnical UniversityXi’anChina

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