Job Description
• Perform cooling flow, and thermal barrier coating investigations.
• Conduct CFD analysis (including RANS, URANS and LES) of combustion systems.
• Identifying improvements in processes and tools, supporting design best practices and develops predictions and methods to validate combustor performance.
• Experience in mid-high pressure combustion testing including test planning, test execution, data post processing and propose design change.
• Conceive ideas to solve aero-thermal design problems and participate in problem solving initiatives
• Lead or participate in organizational efforts in assigned projects and/or tasks
• Participate as a presenter or reviewer in technical and program reviews
• Provide technical guidance to other personnel; mentor others in the organization

Qualifications

Minimum Requirements:
• Minimum of 10 years industrial experience post master's degree in mechanical engineering, aerospace engineering, or related discipline
• Minimum of 5 years of experience with combustion Aero-Thermal design
• Experience with 1D thermo-fluid system simulation software such as Flowmaster.
• Excellent understanding of combustion, emissions associated with gas turbine, ranging from overall component design to detailed understanding aerodynamic and combustion dynamics physics

Desired:
• Experienced as technical leader of combustor development for large frame gas turbine at OEM or equivalent
• Strong interpersonal and leadership skills
• Demonstrated ability in working in a cross-cultural team involving members from all across the globe

Additional Information

All your information will be kept confidential according to EEO guidelines.