Turbine Aerodynamics Lead Engineer

Job Description Summary

The Aerodynamics Lead Engineer will report to the Turbine Aerodynamics Manager and be responsible for leading the design of GE Aerospace’s next generation of turbine components and associated technologies.

Job Description

Essential Responsibilities

• Lead the aerodynamic design and analysis of high- and low-pressure turbine components
• Drive the development of advanced aerodynamic technology to improve engine performance and durability
• Cultivate advanced skills in aerodynamic design, including use of cutting-edge numerical and experimental techniques
• Draw conclusions from component and engine test data to validate aerodynamic designs
• Develop analytical tools/software to improve aerodynamic design and predictive capabilities
• Formulate and execute plans to achieve technical and program requirements
• Develop lean processes to improve organizational productivity and efficiency
• Execute trade studies to meet project requirements, collaborating with horizontal organizations
• Uses some level of judgment and has ability to propose different solutions outside of set parameters but with guidance. Uses prior experience and on-the-job training to solve straightforward tasks. Has access to technical skills and analytic thinking required to solve problems. May use multiple internal sources outside of own team to arrive at decisions.

Qualifications/Requirements

• Bachelor’s Degree from an accredited college/university in Aerospace Engineering or Mechanical Engineering, or related discipline with an emphasis in aerodynamics, aero-thermal, or aeromechanics and a minimum of 3 years of relevant technical experience.

OR

• Master’s Degree from an accredited college/university in Aerospace Engineering or Mechanical Engineering, or related discipline with an emphasis in aerodynamics, aero-thermal, or aeromechanics and a minimum of 2 years of relevant technical experience.

OR

• PhD from an accredited college/university in Aerospace Engineering or Mechanical Engineering, or related discipline with an emphasis in aerodynamics, aero-thermal, or aeromechanics

Desired Characteristics

• Master’s Degree in Aerospace or Mechanical Engineering relevant to turbomachinery aerodynamics with minimum of 3 years of engineering experience OR Doctorate Degree in Aerospace or Mechanical Engineering focused on aerodynamics/compressible flows
• Knowledge of Computational Fluid Dynamics (CFD) and/or aerodynamic testing techniques
• Self-starter, utilizing innovative problem solving to drive solutions on complex issues
• Flexible, friendly, and inclusive; comfortable working in multi-disciplinary global teams
• Demonstrated group facilitation and collaboration skills
• Exceptional communication skills, comfortable preparing and giving impactful technical presentations
• Highly motivated and passionate
• Keen listener and innately driven to succeed

This role requires access to U.S. export-controlled information. Therefore, employment will be contingent upon the ability to prove that you meet the status of a U.S. Person as one of the following: U.S. lawful permanent resident, U.S. Citizen, have been granted asylee or refugee status (i.e., a protected individual under the Immigration and Naturalization Act, 8 U.S.C. 1324b(a)(3)).

Additional Information

GE Aerospace offers a great work environment, professional development, challenging careers, and competitive compensation. GE Aerospace is an Equal Opportunity Employer. Employment decisions are made without regard to race, color, religion, national or ethnic origin, sex, sexual orientation, gender identity or expression, age, disability, protected veteran status or other characteristics protected by law.

GE Aerospace 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 drug screen (as applicable). Employees may also be subject to random and reasonable-suspicion drug and alcohol testing.

Relocation Assistance Provided: No