The Mid-Level Turbomachinery Engineer is responsible for the design, analysis, and optimization of turbomachinery components and systems including turbines, compressors, and rotors. This role leads aerodynamic and structural simulations, supports prototype testing, and collaborates cross-functionally to develop high-performance, reliable turbomachinery solutions for power generation, aerospace, or automotive applications.
Lead design and detailed 3D CAD modeling of turbomachinery components such as blades, vanes, and casings.
Perform and interpret CFD and FEA simulations to optimize aerodynamic efficiency and structural integrity.
Develop test plans, support prototype builds, and analyze performance test data to validate designs.
Collaborate with manufacturing and materials teams to ensure design manufacturability and material suitability.
Participate in design reviews, risk assessments, and root cause analysis for design issues.
Mentor junior engineers and provide technical guidance within the turbomachinery team.
Contribute to technical documentation, standards development, and project management activities.
Advanced aerodynamic and structural design of turbomachinery components
Simulation-driven design optimization and validation
Cross-disciplinary collaboration for manufacturability and performance
Testing, data analysis, and design iteration
Bachelor’s or Master’s degree in Mechanical, Aerospace, or related Engineering field
3–6 years of experience in turbomachinery design, analysis, or testing
Proficient in CAD tools (CATIA, Creo, SolidWorks)
Strong experience with CFD (ANSYS Fluent, CFX, or similar) and FEA (ANSYS Mechanical, NASTRAN)
Solid understanding of fluid dynamics, thermodynamics, and mechanical stress analysis
Knowledge of turbomachinery performance metrics and industry standards
Analytical problem-solving skills with attention to detail
Effective communication and teamwork abilities
Ability to manage tasks independently and lead small projects