Performance Engineer

We are hiring a Performance Systems Engineer with strong expertise in engine performance , thermodynamic modeling , and aero-thermal systems . This role is central to the design, analysis, and validation of gas turbine performance , supporting both new product development and in-service engine support.

Key Responsibilities :

Perform engine performance analysis using thermodynamic models and aero-thermal simulations .

Integrate sub-system predictions into system-level performance models for propulsion systems.

Support and analyze engine performance verification tests , including test planning, execution, and reporting.

Maintain and develop performance modeling tools , data sets , and simulation environments .

Collaborate with cross-functional teams including controls , operability , systems , and hardware design to solve technical challenges.

Deliver technical packages aligned with project milestones, cost, and quality requirements.

Provide in-service engine support , including diagnostics and performance troubleshooting.

Promote continuous improvement in performance engineering tools, methods, and processes.

Communicate complex technical concepts clearly to internal and external stakeholders.

Technical Skills Required :

Strong experience in thermodynamic cycle modeling , engine performance prediction , and aero-thermal analysis .

Familiarity with tools such as NPSS , Python , MATLAB , or similar for performance modeling and data analytics.

Understanding of gas turbine physics , system operability , and transient behavior .

Experience with engine testing , data acquisition , and performance validation .

Knowledge of system engineering principles , robust design , and requirements management .

Excellent communication and documentation skills.

Qualifications :

Bachelor’s or Master’s degree in Mechanical , Aerospace , or Thermal Engineering .

3–10 years of experience in engine performance engineering , thermodynamic modeling , or aero systems .

Experience in gas turbine performance , propulsion systems , or aerospace product development is preferred.