Detailed design and analysis of a flyworthy UAV

Report
Led the comprehensive structural design and system requirements definition for an advanced fixed-wing commercial aerial platform. Executed Global Finite Element Analysis (FEA) to validate the static structural integrity of the airframe under sustained physical loads. The project encompassed the complete mechanical lifecycle, from initial control surface modeling and mechanism design to generating production-ready CAD models and detailed Design for Manufacturing (DFM) 2D drawings.
Published
in Aerospace Engineering 3D Modeling Design Mechanical Engineering
finite-element-analysis computational-fluid-dynamics aeronautics aircraft-design
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