Turbomachinery Aerodynamic Design-Senior Engineer İş İlanı

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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 turbomachines (turbines or compressors) using in house and commercial design tools and will also play a significant role in developing advanced technologies in turbomachinery.

Responsibilities:

  • To study in aerodynamic design and analysis of turbine or compressor stages,
  • To develop aerodynamic design methodologies for turbine or compressor stages,
  • To verify the aerodynamics design, analytical models and tools by using the test results of whole-engine and components,
  • To prepare and present technical data for internal and external customers,
  • Lead and mentor junior engineers.

Qualifications:

  • Education to level in Mechanical Engineering, Aerospace Engineering or a closely related field with strong theoretical background in to turbomachinery principles, thermodynamics, fluid mechanics and heat transfer,
  • At least 5 years of Industrial or Academic experience in aerodynamic design of turbomachinery,
  • Completion of undergraduate/graduate courses relevant to turbomachinery,
  • Experience with turbomachinery design tools (Axstream, Concepts NREC or similar software),
  • Turbomachinery design tool development experience (meanline, throughflow, blade profiling),
  • Experience with the application of commercial CFD codes (ANSYS CFX, FLUENT or Star CCM+)for turbomachinery aerodynamic design and analysis,
  • Ability to use CAD software (CATIA, NX, or similar software.) for basic design purposes,
  • Knowledge of at least one of known programming languages (Fortran, C++, Python etc.),
  • Fluent in English,
  • Aiming a career in aviation,
  • Advanced degree with thesis focused in turbine or compressor aerodynamics field is a plus,
  • Experience in transonic/supersonic flows is a plus,
  • Knowledge with Linux systems is a plus.