Model validation for bird strike crashworthiness

Master Thesis (2024)
Author(s)

M. Post (TU Delft - Aerospace Engineering)

Contributor(s)

Saullo Pereira Castro – Mentor (TU Delft - Group Giovani Pereira Castro)

Wydo van de Waerdt – Mentor (Fokker Aerostructures)

J. J.E. Teuwen – Graduation committee member (TU Delft - Group Teuwen)

Xuerui Wang – Graduation committee member (TU Delft - Aerospace Structures & Computational Mechanics)

Faculty
Aerospace Engineering
Copyright
© 2024 Melvin Post
More Info
expand_more
Publication Year
2024
Language
English
Copyright
© 2024 Melvin Post
Graduation Date
16-02-2024
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Bird strike simulations require accurate information about the nonlinear material properties of the bird and structure, dynamic changes in contact between bird and structure, and large displacements and rotations of the structural elements. The soft-body nature of birds allows it to flow fluidly upon impact, making accurate simulation validation difficult. Setting up a model requires evaluating and considering a large number of parameters. To simplify the process of obtaining validated bird strike models, a set of guidelines for setting up the simulations, covering the major parameters that influence the validation of the models, is established. This was done for an EWVT-SPH (Element Weighted Voronoi Tessellation Smoothed Particle Hydrodynamics) bird model by following the building block approach laid out by the aerospace standards of SAE-G28 for both rigid and complaint target structures.

Files

License info not available
warning

File under embargo until 30-12-2027