Finite element simulation of PMMA aircraft windshield against bird strike by using a rate and temperature dependent nonlinear viscoelastic constitutive model

Author:

Wang Jun,Xu Yingjie,Zhang Weihong

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference17 articles.

1. European Aviation Safety Agency, CS-25.631 Bird strike damage–certification specifications and acceptable means of compliance for large aeroplanes, Annex to ED decision 2011/004/R.

2. McCarty RE, Trudan DE, Davis ON, Three dimensional nonlinear dynamic finite element analysis for the response of a thick laminated shell to impact loads, AIAA85-0713 1985.

3. McCarty RE, Trudan DE, Davis AD. Nonlinear dynamic finite element analysis for the bird impact response of a pre-prototype T-38 aircraft windshield system. In: 15th conference on aerospace transparent materials and enclosures. Monterey, CA; 1989.

4. Boroughs RR. High speed bird impact analysis of the Learjet 45 windshield using DYNA3D. In: 39th AIAA/ASME/ASCE/AHS/ASC structures, Structural dynamics, and materials conference and exhibition. Long Beach, CA; 1998.

5. Experimental and fem study of windshield subjected to high speed bird impact;Yang;Acta Mech Sinica,2003

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