Oguz Durmaz

- Flight envelope definition - Guidance regarding loads analysis for the preliminary design phase. - Conducting comprehensive loads analysis to ensure structural integrity and compliance with regulatory standards across flight conditions. - Managing weight distribution and balance optimization. - Utilizing advanced computational tools and simulations to guide the design and operational decisions. - Driving innovation in flight physics methods and tools to improve analysis accuracy and efficiency. - Aircraft water loads analysis, hull and float loads - Development of the landing gear loads model, calculation of the reaction forces and unbalanced moments. - Definition of MoCs for the loads-related certification basis. - Performed ground handling loads analysis and created tailored tools for compliance with CS-23.

- Led tool development initiatives for conceptual aircraft and ground/landing loads analysis using Python, ensuring project alignment with technical requirements. - Conducted and managed aircraft loads analysis for the flight demonstrator, coordinating cross-functional teams for optimal performance. - Reviewed and refined loads and dynamics requirements, contributing to strategic planning and execution.

- Directed and mentored the Loads team on the TF-X project, fostering a collaborative and productive work environment. - Ensured accurate loads calculation during the preliminary design phase, setting the technical direction for team members.

- Compliance verification engineering (CVE) of the loads for a modification project certification process. - Supplemental type-certificate is planned to get from the authority after the modifications of the aircraft. - Responsibility for the certification strategy with regards to aircraft loads - Coordination with airworthiness engineers to define the MoC’s and the applicability of CS-25 requirements on the modifications of the aircraft.

- Tool development for the aircraft loads analysis - Generating the V-n diagrams - Contributing on the studies for control surface hinge moment estimations - Defining the flight conditions for the trim – simulation analysis. - Critical load case determination - Defining the load cases for the static test of the aircraft - Generating aerodynamic database for load calculations from wind tunnel and CFD results by using in-house tools developed by our team - Aerodynamic, inertia and miscellaneous loads modeling - Constructing loads model and preparing loads analysis reports - Verification of the loads analysis with flight tests (Flight load survey) - Matching the maneuvers of the aircraft and the fatigue spectrum within aircraft structural integrity program - Critical design experience on CS – 23 - Preparation of EASA certification reports to meet regulatory requirements

Research Student, Environmental and Applied Fluid Dynamics Department - Dynamic Stall investigation of flapping wing by using PIV measurement technique

- Modeling of the fluid flow and flow control