This work describes the basic assumptions of the analyses, i.e. bird properties, composite failure modes, and the way in which the simulations have been carried out in an industrial environment. Numerical simulations were able to predict that the bird did not penetrate the leading edge skin. The final correlation between numerical and experimental showed that good correlation was achieved.
Study, design and testing of structural configurations for the bird-strike compliance of aeronautical components / Guida, M.. - (2008).
Study, design and testing of structural configurations for the bird-strike compliance of aeronautical components
M. Guida
2008
Abstract
This work describes the basic assumptions of the analyses, i.e. bird properties, composite failure modes, and the way in which the simulations have been carried out in an industrial environment. Numerical simulations were able to predict that the bird did not penetrate the leading edge skin. The final correlation between numerical and experimental showed that good correlation was achieved.File in questo prodotto:
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