Optimization of geometry and laminate for corrugated plate for aircraft wing morphing

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Experience Level: Expert
The topic is '' Optimization of geometry and laminate for corrugated plate for aircraft wing morphing''. In this project following things have to be determined
-Determine the size n shape of the corrugation to withstand certain aerodynamic loading
-Derive the geometric properties analytically n compare with FEM (finite element model) by using different materials (metallic n CFRP). .

The optimization and FEM should be carried out using MSC Software (Nastran & Patran) or ANSYS

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