Onur Sevindik

- During the two-day competition, helped set up and maintain the overall organization.

- Aerodynamic Design & CFD: Optimized WIG airframe and wing geometry and validated low-altitude lift and stability through CFD analysis. - Prototype Build & Deployment: Planned, manufactured, and assembled a 4-m wingspan aircraft prototype and successfully delivered it to IDEF 2025 within 30 days

- Aerodynamic design & CFD analysis of airframes for flight performance and stability - Mechanical & structural design ensuring integrity and safety compliance - Rapid prototyping, manufacturing & assembly - Planned, led & evaluated test flights; analyzed data for design improvements - Operated off-the-shelf & in-house UAVs for external client test flights, ensuring compliance

- Requirements Definition: Determined software and hardware requirements for a test platform built to evaluate UAV propulsion systems. - Software Design and Development: Designed and developed the software for the platform's operation per defined specifications. - Hardware Design: Defined the electronic hardware design and selected required components. - Testing and Validation: Ran a series of tests to verify correct software and hardware functioning.

- Volunteer research project assistant in a TUBITAK Project - Researching about controlling the deformable space reflectors using intelligent control techniques

- Took CAD training to be able to do basic technical drawing - Responsible for the structural design and production of the given internship project - Had the opportunity to make observations about engineering management and general operation

- Observing the Factory Level Maintanence operations

Completed a four-year, fully English-taught Bachelor's program in Aerospace Engineering, covering aerodynamics, flight mechanics, propulsion, aerospace structures, and control systems. Academic projects include a TÜBİTAK-supported study on intelligent control of deformable space reflectors (advisor: Dr. Ipar Ferhat) and an optimization-based stability augmentation system design for the F-16 (advisor: Prof. Dr. Ozan Tekinalp).