Abstract:

This study focuses on the modeling and static structural analysis of a fuselage lattice structure using aluminum alloy materials. The fuselage is an essential component in aircraft design, where it must maintain a balance between strength, weight, and flexibility. The lattice structure is an efficient design approach, known for its ability to withstand high stresses while keeping the overall weight low. Aluminum alloys are widely used in aerospace applications due to their excellent strength-to-weight ratio and durability.

Description:

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