Bird strike is a severe high velocity impact load case for all forward-facing aircraft components and a major design driver due to the high energies and the strict safety requirements involved. This paper summarises an experimental and numerical study to design a bird strikeproof lightweight metallic Krueger flap as a high-lift device concept for a laminar wing leading edge of a single aisle short range aircraft. The whole design process was based on numerical optimisations for static load cases in combination with high velocity bird impact simulations, with the focus on accurate modelling of the fluid-like bird projectile, the plasticity of the aluminium material and the failure behaviour of the structural hinges and fastened joints.
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