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This project is dedicated to validate and optimize the structural strength of the spars in wing

Teknofest 23-24 Rocket simulations of UBT High-Shool Rocket Team.

CAE - FIME - UANL - AF1 - Análisis Estático Lineal

we have to calculate stress using FEA method and see when maximum stress is occured.

we have to modify some new parameters in a part and give different boundary conditions and mesh.

We have  to analize through  a  FEA method  .

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