Smooth Particle Hydrodynamics Birdstrike Analysis on Aircraft Wing Leading Edge
(2021)
Journal Article
Hampson, P., & Talhah, I. (2021). Smooth Particle Hydrodynamics Birdstrike Analysis on Aircraft Wing Leading Edge. International Journal of Multiphysics, 15(3), 291-309. https://doi.org/10.21152/1750-9548.15.3.291
Aircraft wing leading edges subjected to simulated birdstrike impact was investigated using the finite element ANSYS Autodyn solver. The bird was modelled using a Smooth Particle Hydrodynamics (SPH) method. Two validation studies were conducted prior... Read More about Smooth Particle Hydrodynamics Birdstrike Analysis on Aircraft Wing Leading Edge.