Impact Simulation With an Aircraft Wing Using SPH Bird Model
Journal Title: INCAS BULLETIN - Year 2015, Vol 7, Issue 3
Abstract
The work presents an approach to simulate a model bird-strike on an aircraft wing using Lagrange mesh free method in Autodyn. The presented SPH model has been used to simulate a threedimensional impact of the bird with the aircraft wing, at different angles, at a velocity of 262,22m/ s. The bird was modeled as a fluid cylinder with two hemispherical ends representing a commonly used shape in the numerical studies of bird strike. The main objective was to identify the safe impact velocities for which the wing is not damaged.
Authors and Affiliations
BELEGA Bogdan-Alexandru
Keywords
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- EP ID EP89933
- DOI 10.13111/2066-8201.2015.7.3.5
- Views 123
- Downloads 0
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