Finite Element Method on CBA123 Design and Certification

Paper #:
  • 921445

Published:
  • 1992-11-01
Citation:
Fontes, R., "Finite Element Method on CBA123 Design and Certification," SAE Technical Paper 921445, 1992, https://doi.org/10.4271/921445.
Pages:
11
Abstract:
The finite element method was intensively used by EMBRAER for the aircraft CBA123 - Vector, design and certification (FAR 25).This method together with in house developed pre-and pos-processors were very usefull tools for linear and non-linear stuctural, fatigue, composite structure and damage tolerance analysis.The substantiation of the analysis method was based on past experience and on components, sub-components and full scale instrumented tests.
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