Engine Aerodynamics Design Engineer

GENERAL QUALIFICATIONS

• Graduates of universities with degrees in Aerospace, Aeronautical, or Mechanical Engineering,
• Knowledgeable in the design, analysis, and optimization of gas turbine engine components (compressors, turbines, combustion chambers, etc.),
• Strong theoretical background in Thermodynamics, Aerodynamics, Heat Transfer, Fluid Mechanics, and Computational Fluid Dynamics,
• Proficient in using at least one CFD program such as Ansys Fluent, Ansys CFX, or OpenFOAM,
• Proficient in using at least one CAD program such as CATIA or SpaceClaim,
• Preferably knowledgeable about gas turbine engine performance calculations (e.g., GasTurb),
• Preferably experienced with 1D flow modeling and design tools,
• Preferably skilled in any programming language (MATLAB, Python),
• Advanced technical English proficiency,
• Open to new developments and continuously inclined towards self-improvement,
• Strong communication skills, capable of working individually and as part of a team,
• Able to develop new approaches to problem-solving and think analytically,
• Capable of creating clear and understandable reports in accordance with company procedures.

JOB DESCRIPTION

• Participate in the conceptual and detailed aerodynamic design of gas turbine engines,
• Create the main flow path for assigned components, and perform airfoil design and analysis,
• Carry out aerodynamic and thermodynamic design, analysis, and optimization work for gas turbine engine components,
• Develop performance curves and maps for components and evaluate performance characteristics,
• Contribute to the development of aerodynamic design and analysis methodologies,
• Monitor the testing activities of assigned components, validate test results, and perform development work,
• Report technical work in accordance with company procedures,
• Collaborate with other engineering disciplines.