Engine Structural Analysis Simulation and Modeling Engineer

General Qualifications

• Graduated from Mechanical, Aerospace, Aeronautical, Manufacturing, Automotive or Mechatronics Engineering departments,
• Possesses a strong theoretical background in strength of materials, heat transfer, statics, dynamics, vibration, fatigue, and materials science,
• Experienced in Finite Element Analysis (preferably with ANSYS),
• Proficient in engineering software such as ANSYS, MATLAB, and CAD tools,
• Knowledgeable about gas turbine engine operating principles, and component behavior under high-temperature, vibration, and mechanical stress conditions,
• Technically competent and fluent in technical English with an understanding of aerospace standards and regulations (e.g., FAA, EASA, MIL, SAE),
• Skilled in general engineering tools and software (e.g., MS Office),
• Follows industry developments and has an innovative mindset,
• Able to work in coordination with other teams related to areas of responsibility,
• Strong communication skills and a good team player.

Preferred Qualifications

• Holds an M.Sc. or Ph.D. degree in Mechanical, Aerospace, Aeronautical, Manufacturing, Automotive or Mechatronics Engineering,
• Knowledgeable in structural analysis, structural optimization, and load distribution of engine components,
• Experienced in LCF and HCF fatigue analyses, thermo-mechanical fatigue, and creep analyses,
• Familiar with rotor dynamics concepts such as Campbell diagrams, Bode plots, critical speeds, and mode shapes,
• Experienced in multi-body dynamics and fluid–structure interaction (FSI) analyses,
• Experienced in thermal, static, modal, and harmonic modules of finite element analysis software,

We are looking for a “Engine Structural Analysis, Simulation and Modeling Engineer” who possesses the above qualifications to join our team.

Job Description

• Assignments will be made considering project dynamics and may include the following responsibilities:
• Performing overspeed, overtemperature, and burst analyses of rotating components in gas turbine engines in accordance with engine regulations,
• Conducting structural integrity analyses of engine structures in blade-off scenarios,
• Investigating the thermal and mechanical behavior of rotating components under operating loads to determine tip clearances,
• Determining critical loading conditions and requirements for turbofan engine components considering high maneuverability of aircraft,
• Modeling high-speed aerospace bearings, determining stiffness and damping coefficients as a function of speed, performing macro and micro modifications, and conducting life estimations according to mission profiles,
• Performing component-level analyses during the conceptual design stages of new engine architectures to guide detailed design studies,
• Preparing documentation for all analysis, simulation, and modeling activities,
• Collaborating with design teams to develop and improve engine components that meet system-level requirements and performance targets,
• Supporting analysis–test correlation activities to validate system performance and identify areas for improvement,
• Contributing to the identification of potential risks in system design and operation, and developing strategies to ensure engine reliability and safety through weight reduction, material selection, additional safety measures, and design modifications.