Profile
Lead Structural Analysis Engineer at Turkish Aerospace Industries (TAI), working on metallic and composite aircraft primary structure since 2017 (9+ years). The work covers the whole stress discipline: static strength and stability, fatigue and damage tolerance, composite and lightweight design, GFEM-based sizing and structural optimisation. Currently leads the durability and damage tolerance (DaDT) work package on a fighter-jet programme and, since late 2025, analysis method and tool development in the stress group. Earlier work covers EASA CS-23 certification stress analysis on the Hürkuş trainer (forward fuselage, and the rudder weight-reduction study), GFEM-based sizing of fighter primary structure, and preliminary landing-gear and eVTOL structural studies. Day to day that means stress reports taken through release, sizing and weight trade studies, crack-growth and fail-safe assessments, and non-conformance dispositions agreed with the loads, design and test teams.