DOI QR코드

DOI QR Code

Design criteria for birdstrike damage on windshield

  • Marulo, Francesco (Department of Industrial Engineering - Aerospace branch, University of Naples "Federico II") ;
  • Guida, Michele (Department of Industrial Engineering - Aerospace branch, University of Naples "Federico II")
  • 투고 : 2013.11.27
  • 심사 : 2014.01.19
  • 발행 : 2014.03.25

초록

Each aircraft have to be certified for a specified level of impact energy, for assuring the capability of a safe flight and landing after the impact against a bird at cruise speed. The aim of this research work was to define a scientific and methodological approach to the study of the birdstrike phenomenon against several windshield geometries. A series of numerical simulations have been performed using the explicit finite element solver code LS-Dyna, in order to estimate the windshield-surround structure capability to absorb the bird impact energy, safely and efficiently, according to EASA Certification Specifications 25.631 (2011). The research considers the results obtained about a parametric numerical analysis of a simplified, but realistic, square flat windshield model, as reported in the last work (Grimaldi et al. 2013), where this model was subjected to the impact of a 1.8 kg bird model at 155 m/s to estimate the sensitivity of the target geometry, the impact angle, and the plate curvature on the impact response of the windshield structure. Then on the basis of these results in this paper the topic is focused about the development of a numerical simulation on a complete aircraft windshield-surround model with an innovative configuration. Both simulations have used a FE-SPH coupled approach for the fluid-structure interaction. The main achievement of this research has been the collection of analysis and results obtained on both simplified realistic and complete model analysis, addressed to approach with gained confidence the birdstrike problem. Guidelines for setting up a certification test, together with a design proposal for a test article are an important result of such simulations.

키워드

참고문헌

  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.
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피인용 문헌

  1. Soft impacts on aerospace structures vol.81, 2016, https://doi.org/10.1016/j.paerosci.2015.11.005
  2. Numerical analysis of collision of the multimaterial bird model with helicopter windshield vol.42, pp.1, 2014, https://doi.org/10.1515/jok-2017-0015
  3. Application of mathematical modeling for certification of superjet-100 airplane vol.2, pp.2, 2014, https://doi.org/10.1007/s42401-019-00029-7
  4. A Sensitivity Analysis of the Damage Behavior of a Leading-Edge Subject to Bird Strike vol.10, pp.22, 2014, https://doi.org/10.3390/app10228187
  5. A review of the bird impact process and validation of the SPH impact model for aircraft structures vol.129, pp.None, 2022, https://doi.org/10.1016/j.paerosci.2021.100787