- Propose changes in the layup to reduce defects and improve cycle time.- Structural analysis of the layup changes.- Support on structural changes on the blade.

-Define design rules/limits-Define manufacture tolerances and defect limits.-Design subcomponent specimens to test thickness tolerances.-Perform DFMEAs.-Support on nonconformance evaluation and repair definitions.-Support on material qualifications.

-Define manufacture tolerances and defect limits.-Propose layup changes to reduce defects and improve cycle time.-Perform DFMEAs.-Support on subcomponent test for wrinkles limits.-Support on nonconformance evaluation and repair definitions.-Support on material qualification.

- Composites specialist- Structural analyst

• Developed a non-linear material model to simulate quasi-static and fatigue damage propagation in composite materials. • Implemented the model into Abaqus/Explicit subroutines.• Reduced the error on the estimation of the strain energy release rate from 20% to 2%.• The crack growth rate was accurately estimated with an error of only 2.5%• Supported two master students on the application of the proposed model on the analysis of fibre-reinforced stiffened panels.

Participated at SAE Brazil AeroDesign student competition in the Advanced category where was developed an unmanned cargo aircraft, from the conceptual design to competition flights.2017: • Performed structural analysis of sandwich-structured composite components (wingspars and main landing gear) and metallic components (wheels) using FEMAP with NX Nastran. • Received Honorable Mention for the best project in the Advanced category.2016: • Performed structural analysis of the wing spars and main landing gear (constructed in laminated composites). • Optimised these components reducing the mass by 9% using Altair HyperMesh and OptiStruct. • Achieved 2nd place in the Altair Optimisation Challenge.

Participated at SAE Brazil AeroDesign student competition in the Regular category • Supported the team in the design and stress analysis of the aircraft's structures. • Performed structural analysis of the aircraft’s wing spars and twin-boom.