QUALIFICATIONS AND JOB DESCRIPTION
Job Description:
The successful candidate will take part in Aerodynamic Design of gas turbine engine components in Concept, Preliminary and Detailed phases and will collaborate with engineering disciplines.
The successful candidate will design state of the art gas turbine engine components (diffuser, nozzle, etc.) using in house and commercial design tools and will also play a significant role in developing advanced technologies in aerodynamics.
Responsibilities:
- Study in aerodynamics design and analysis of gas turbine engine components,
- Develop aerodynamics analysis and design methodologies,
- Verify the aerodynamics design, analytical models and tools by using the test results of whole-engine and components,
- Plan and participate ground testing of aerodynamic related components for validation and verification purposes,
- To prepare and present technical data for internal and external customers,
- Provide guidance and support to designers to optimize aerodynamic performance,
- Having ability to think strategically and solve problems,
- Collaborate cross functionally with design, development and test groups.
Qualifications:
- BSc. degree in Mechanical Engineering, Aerospace Engineering or a closely related field with a solid knowledge of thermodynamics, fluid mechanics and heat transfer,
- At least 5 years of industrial or academic experience in aerodynamics field,
- Solid experience on subsonic/supersonic compressible flows applicable to diffuser, nozzle or similar geometries,
- Solid experience with commercial CFD codes (ANSYS CFX, FLUENT or Star CCM+),
- Ability to use CAD software(CATIA, NX etc.) for basic design purposes,
- Code development skills with one of known programming languages (Fortran, C++, Python etc.),
- Fluent in English,
- Aiming a career in aviation,
- Knowledge with Linux systems is a plus,
- Experience with High Performance Computing systems is a plus,
- Advanced degree with thesis focused in computational aerodynamics field is a plus.
