Abdulkadir Cekic

•According to ECSS standards, perform quasi-static, modal, global buckling, frequency response, and thermo-elastic analysis of satellites in TURKSAT 6A and Small Geo project. •Participate in system and subsystem level requirement generation in line with ECSS standards and complete SRR and PDR successfully in Small GEO project. •Successfully complete mechanical qualification test campaign and evaluate mechanical test results in the TURKSAT 6A project.

• Participate in various finite element methodology development projects with FORD of Europe and FORD of North America. •Perform linear, non-linear, and frequency response analysis of engine components, including non-linear material and contact modeling. •Carry out thermo-mechanical, dynamic, and low cycle-high cycle fatigue analysis of engine components such as exhaust manifold of Ecotorq engines, the after-treatment system.

•Develop scripts to calculate aerodynamic and inertial loads on the aircraft, mainly written in FORTRAN, C, Visual Basic, and MATLAB. •Performed detailed structural load analysis by using the developed script in “ANKA” Unmanned Air Vehicle Project, “HURKUS” Basic Trainer Aircraft Project, and “SIMSEK” High-Speed Target Drone Project. •Generate dynamic model of “HURKUS” basic training aircraft and performed modal analysis by using MSC PATRAN-NASTRAN.