Validation of Numerical Methodologies with Experimental Bird Strike Data for Leading-Edge Damage Assessment.

I have conducted a numerical simulation of an experimental study on bird strike analysis, employing two distinct methods: Smoothed Particle Hydrodynamics (SPH) and the Coupled Eulerian-Lagrangian (CEL) approach. The aim of the study was to evaluate and compare the performance of these methods in replicating the experimental results. Both methodologies were analyzed in terms of accuracy, computational efficiency, and their ability to model the structural response during the bird strike event. This comparative study provides insights into the advantages and limitations of each method, contributing to the ongoing development of reliable numerical simulation techniques for aerospace impact analyses

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