Gizem Algül

• Experienced in flight test and certification for fixed wing aircraft • Perform test readiness reviews and witness qualification tests • Knowledge of EASA CS-23 Certification Specifications for Normal, Utility, Aerobatic and Commuter Category Aeroplanes • Perform longitudinal, lateral and directional static and dynamic stability assessments of the fixed wing aircraft • Experienced in aerodynamics and stability characteristic of the aircraft during low speed, transonic speed and high speed • Perform horizontal/vertical stabilizer sizing assessments based on center of gravity positions and longitudinal instability limits • Perform assessment for enhancement of the aerodynamic and stability characteristics of the aircraft during flight test and development phase • Participated in the Concept Development, Planform Selection and Alternative Selection Review phases of a fighter aircraft project • Participated in low and high speed wind tunnel tests of a fighter aircraft project for the aerodynamic and static stability characteristics during concept development phase

• Experienced in flight test and certification for aircraft/store compatibility tests • Knowledge of MIL-HDBK-1763 Aircraft/Stores Compatibility: System Engineering Data Requirements and Test Procedures • Participated in the Inflight Loads, Jettison and Employment tests of aircraft/store configurations for several projects • Perform assessment of the weight and geometry limits of the missile as a systems requirement for the integration to the air planforms within the concept development phase of a missile project

Thesis: Buffet Investigation on Airfoils