30th Congress of the International Council of the Aeronautical Sciences

03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS

G.C. Fonseca, Embraer, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil

The focus of this work is the development of a manufacturing methodology of thick composite laminated components for aeronautical applications. The following points were accomplished: lug conception, mold design and component manufacturing. Lug conception was accomplished by numerical analysis used to determine the thickness and geometry under a load condition for a specific structural application


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