GE is an equal opportunity employer, offering a great work environment, challenging career opportunities, professional training and competitive compensation.
As a Computational Heat Transfer Engineer, you will innovate, design, build, and integrate the next generation cooling technologies into Aviation and Power Generation Gas Turbines.
- Develop and apply advanced flow and heat transfer technology, including design tools and processes, in order to meet the technical and competitive challenges of GE turbomachinery products.
- Perform CFD calculations on complex geometries to understand detailed flow physics, leading to improved turbine design life
- Participate in identifying, planning and developing conceptual designs for advanced cooling technologies for gas turbines and turbomachinery products.
- Doctorate degree in Mechanical Engineering, Aerospace Engineering, or related disciplines OR Master’s degree (with thesis) in Mechanical Engineering, Aerospace Engineering, or related disciplines with at least 3 years of post-degree experience in Heat Transfer or Fluid Dynamics Design or Analysis.
- Expertise in the application of 1D, 2D and 3D Heat Transfer or Fluid Dynamics design and analysis methods.
- Ability to develop innovative solutions to Heat Transfer related problems
- Legal authorization to work in the U.S. is required. We will not sponsor individuals for employment visas, now or in the future, for this job opening.
- Must be willing to work out of an office located in Niskayuna, NY.
- Must be willing to take a drug test and submit to a background investigation as part of the selection process.
- Must be 18 years or older.
- You must submit your application for employment on the careers page at www.gecareers.com to be considered.
Additional Eligibility Qualifications
GE will only employ those who are legally authorized to work in the United States for this opening. Any offer of employment is conditioned upon the successful completion of a background investigation and drug screen.
This position is eligible for The Double Rewards Employee Referral Program
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- Post-Doctorate experience and/or two plus years of experience in turbomachinery research.
- Domain knowledge in gas turbine design and gas turbine cooling technologies.
- Experience in numerical methods development, such as reduced order models and 3D CFD algorithms
- Superb communication skills.
- Strong publication record in the gas turbine heat transfer community.
- Experience in experimental heat transfer methods, as applied to gas turbine airfoil design.
- Experience with combustion and reacting flows.
- Project leadership experience, including successful track of completing deliverables on schedule and on budget.
- Excellent work ethic, and able to work well with broad and diverse teams.
- Demonstrated dedication to completing jobs on time and on budget.
Section 19 Job
YOU MUST BE ABLE TO SATISFY THE REQUIREMENTS OF SECTION 19 OF THE FEDERAL DEPOSIT INSURANCE ACT.
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