Tytuł pozycji:
Numerical simulations of a bird strike against a helicopter windshield
The article presents simulation results of a bird strike with a helicopter windshield of small helicopter category. It
turns out that there are no certification requirements regarding windshield of this category. Therefore Agusta A109
helicopter as a representing this helicopter category has been chosen for researcher. The simulations were conducted
on the basis of LS-DYNA software by means of the SPH method for bird model shape of cylinder with hemispherical
endings for the speed of Vc = 285 km/h. The analyses regarded various angles of the bird model impact into
windshield. As a result of the simulations, comparative analyses in the aspect of time curves of the kinetic energy,
velocity, and windshield deformation were achieved. The analysis shows that at smaller angles of attack, the bird’s
model has a higher speed at the moment of impact, and thus greater kinetic energy, because it did not lose speed as
a result of the collision. In addition, the deflection of the windshield is smaller. In some cases, the deflection of the
windshield may be observed, which indicates the elastic response of the system. In case of impact in the normal
direction to the surface of the glass, the bird’s model practically pierces it. The use of a thicker pane translates into
less deformation of the pane, but causes its destruction at the connection point with the helicopter carrier structure.