Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation
Open Access
- 31 December 2007
- journal article
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 20 (6) , 511-517
- https://doi.org/10.1016/s1000-9361(07)60075-2
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
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- High speed bird impact analysis of the Learjet 45 windshield using DYNA3DPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Three dimensional nonlinear dynamic finite element analysis for the response of a thick laminated shell to impact loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985