Aircraft Conceptual Development Engineer

EXPLANATION

As a part of the Flight Mechanics and Conceptual Development team of our Flight Sciences Department, you will have the opportunity to contribute to the development of new aircraft systems, also you will be involved in the flight mechanics analysis processes of the aircraft systems.
The selected engineer will play a role in defining the performance and mission duty requirements of new aircraft during the conceptual development phase, as well as creating design alternatives that provide specified requirements, and selecting the most optimal design in terms of performance, aerodynamics, control and stability. Within the studies of flight mechanics, you will ensure to identify stability-control processes for aircraft, and determining trim and control strategies. To complete the tasks given, you will carry out the software development for the computational tools that are required and will be involved in CFD analysis processes.
Our teammate is expected to be highly motivated, adaptable to dynamic working conditions, self-sufficient, and possess understanding of especially the military aviation and defense sectors.

GENERAL FEATURES

• Graduated from the Aeronautics, Astronautics, Aerospace or Mechanical Engineering departments.
• Preferably has a master’s degree in these departments.
• Has a very good level of flight dynamics, aerodynamics, propulsion systems and flight control background.
• Has a very good background in mathematics and physics.
• Understanding of Computational Fluid Dynamics (CFD) analysis methodologies.
• Interested in the development processes of conceptual aircraft.
• Very good knowledge of at least one of the scientific programming languages.
• Should be interested in the aviation and defense industry.
• Will be able to work efficiently both individually and as a team.
• Has a self-sufficient and goal-oriented work style.
• We are looking for teammates who can adapt to a fast-paced work environment.

 

JOB DESCRIPTION

• Validation and development of aircraft flight mechanics analysis methods.
• Development of stability and control analysis systems for aircraft during the R&D and product development phases.
• Analyzing aircraft flight test data, examining special situations seen in the tests.
• Determination of operational, performance and weight requirements of the conceptual aircrafts.
• Design and optimization studies of conceptual aircraft components/sub-components.
• Obtaining basic aerodynamic parameters of conceptual aircraft using CFD modelling methods.
• Supporting other teams on issues in flight analysis, performance simulations, flight control, etc.
• Preparation of flight mechanics and conceptual aircraft development documents.