The FEM Analysis on the Damage of Wing Leading Edge under Hail Impact

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Abstract:

The low and medium speed impact damage of composite structure of wing leading edge under hail impact is examined by numerical simulations, using nonlinear dynamic finite element analysis software LS-DYNA. For different impact velocities, the dynamic responses of wing leading edge are obtained and the damage in composite panel is clearly demonstrated. The relations of impact energy, maximum displacement and the damage state are analyzed. The simulation results can provide some references for the design of wing leading edge.

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330-333

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February 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] A.G. Hanssen, Y. Girard, L. Olovsson, T. Berstad, M. Langseth: International Journal of Impact Engineering Vol. 32 (2006), p.1127.

DOI: 10.1016/j.ijimpeng.2004.09.004

Google Scholar

[2] L. Wu, Y.N. Guo, Y.L. Li: Explosion and Shock Waves Vol. 29(6), 2009, p.642.

Google Scholar

[3] LS-DYNA3D key word user's manual[M]. Livermore Software Technology Corporation. Version 971, (2007).

Google Scholar

[4] M. Anghileri, L.M. L. Castelletti. International Journal of Impact Engineering Vol. 31 (2005), p.929.

Google Scholar

[5] Z. Shen, Z.L. Zhang, J. Wang: Acta Materiae Compositae Sinica. Vol. 21(5), 2004, p.140.

Google Scholar

[6] N.B. Yang: Composite Structural Design For Aircraft. Aviation Industry Press (2004).

Google Scholar

[7] Q.Y. Cheng, X.Y. Tong: Mechanical Science and Technology for Aerospace Engineering Vol. 27(11), 2008, p.1311.

Google Scholar