About the role
Key Responsibilities:
• Carry out gas turbine turbomachinery aerodynamic design and analysis activities.
• Carry out design & off-design analysis, post-process engine test data, liaise with internal and external stakeholders.
• Provide technical leadership in engine architectural studies
• Develop numerical and experimental methods for method verification and validation
• Define individual and team performance metrics, monitor the performance, and provide constructive feedback
• Review the designs, simulations and generate testing guidelines • Identify project risks and plan for mitigation
Qualifications & Experience
• Aerospace, Mechanical Engineering degree or a related field.
• Strong background in gas turbine propulsion, turbomachinery design, thermodynamics and fluid mechanics.
• Hands-on experience in axial and centrifugal compressor, turbine design and optimization for gas turbine applications.
• Experience in unsteady modelling, bleed flows, compressor stability, casing treatment and sub-idle modelling will be considered as plus.
• Fluent in English
• Experience: 5-15 years or more.
Skills
• Technical skills in one or a combination of stated topics.
• Using commercial turbomachinery tools such as Concepts NREC, AxStream or similar.
• Experience in CFD or through flow simulation methods. Ansys CFX, Numeca/Cadence, Fluent etc.
• Experience in multi-point and multi-disciplinary optimization • Experience in programming using C, Matlab/Simulink or similar.
• Experience in coatings, and cooling technologies.
• Awareness on the state-of-the-art technologies in materials, heat transfer and structural mechanics to link with aerodynamic design and performance
• Good communication and presentation skills to interact with team members, clients, and vendors.
• Ability to solve problems, prioritize tasks and delegate when necessary