Smooth Particle Hydrodynamics Birdstrike Analysis on Aircraft Wing Leading Edge
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 to the main investigation. The first simulated im...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
MULTIPHYSICS
2021-07-01
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| Series: | International Journal of Multiphysics |
| Online Access: | http://journal.multiphysics.org/index.php/IJM/article/view/749 |