Critical parameters like HUGONIOT pressure and Stagnation pressure are compared from each study. Results are compared with published literature based on the standard experimental data. First part of current research aims at bring out comparison between analysis methods along with their pros and cons, the Explicit analysis capabilities of Abaqus were used for modeling the phenomenon using three methods LAGRANGIAN, COUPLED LAGRANGIAN-EULERIAN (CEL) and SMOOTH PARTICLE HYDRODYNAMICS (SPH). ![]() ![]() Current paper addresses relevant issues for today’s industry towards a universally accepted method of bird strike analysis Finite element based computational methods. A FE model for fastener failure and fastener hole embrittlement. ![]() There has been significant research done on various ways of doing bird strike simulation, till date Aerospace & defense Industry is concerned with two key issues 1.Comparative assessment of available methods 2. Bird strike Simulation helps in assuring aircraft safety, in eliminating cost & effort required for practical tests.
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