Job Description Summary

Job Description

Essential Responsibilities

• Lead the aerodynamic design and analysis of high- and low-pressure turbine components
• Perform advanced aero-thermal computational fluid dynamics analyses
• Provide technical guidance and domain expertise across cross-functional teams, including collaboration with engineering, manufacturing, quality, supply chain, and operational partners.
• Execute and support technical deliverables, including design reviews, process improvements, product support activities, safety initiatives, and operational problem resolution.
• 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
• Leads program issue resolution efforts to meet customer and/or regulatory expectations across organization
• Partner with organizational stakeholders and functional teams to support execution of technical priorities, strategic initiatives, and operational goals.
• Strong coaching, mentoring, and training skills within the domain, site, or organization, with a focus on engaging early-career personnel..

Qualifications/Requirements

• 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.
• Master’s Degree from an accredited college/university in Aerospace Engineering or Mechanical Engineering, or related discipline with an emphasis in turbomachinery aerodynamics, and a minimum of 9 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 turbomachinery aerodynamics, and a minimum of 8 years of relevant technical experience. 

DESIRED CHARACTERISTICS:

• Master’s Degree in Aerospace or Mechanical Engineering relevant to turbomachinery aerodynamics with minimum of 9 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 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.