Develop and own cycle and performance models (steady-state and transient) for engines across the operating envelope
Predict thrust/power, fuel flow, temperatures, pressures, and margins versus altitude, Mach, and mission conditions
Plan and support engine performance testing, including defining test matrices and key performance points
Correlate test data to models, perform uncertainty analysis, and update maps/models based on results
Create and refine component maps and limits (fan/compressor/turbine maps, operating lines, surge and temperature margins)
Collaborate with controls engineers on schedules (VGV, bleeds, fuel flow) to balance performance, operability, and hardware life
Analyze fleet and in-service performance data to identify trends, degradation, and improvement opportunities
Lead performance trade studies and optimization for efficiency, fuel burn, and operating margins
Support certification and customer programs with validated performance data and technical justifications
Provide technical leadership and mentoring to junior engineers and drive best practices in thermodynamic performance
Work cross-functionally with design, aero, mechanical, systems, test, and services teams to ensure performance requirements are met
Improve gas turbine thermodynamic and operability modeling techniques
Engage in research, design, development, and enhancement of technologies to improve performance, operability, and cost
Develop strong relationships with external customers and partners
Document technical data and results in accordance with engineering policies and procedures
Communicate significant technical issues, risks, or developments in a timely manner
Participate in organizational initiatives and technical/program reviews
Support technical program managers and mentor less experienced engineers
Make decisions within a defined framework and engage senior team members on complex issues
Contribute independently to projects while supporting senior engineers in advancing performance related technologies

Requirements

Bachelor's degree in engineering from an accredited university or college
Minimum of 8 years' experience related to Aircraft Engine Performance or related discipline
Advanced degree in Mechanical or Aerospace Engineering with focus on thermofluids or turbomachinery (desired)
Enthusiasm for propulsion and aero/thermodynamic disciplines
Experience in aircraft engine testing, cycle performance, or component aero design
Proficiency with NPSS, Python, or similar simulation/programming tools
Experience in gas turbine engine test support, analysis, and thermodynamic modeling
Experience in engine qualification and certification
Ability to obtain and maintain a U.S. Government Security Clearance (U.S. citizenship required)

Benefits

Healthcare benefits include medical, dental, vision, and prescription drug coverage
Access to a Health Coach from GE Aerospace
Employee Assistance Program, providing 24/7 confidential assessment, counseling, and referral services
Retirement benefits include the GE Aerospace Retirement Savings Plan and a 401(k) savings plan with company matching contributions and retirement contributions
Access to Fidelity resources and planning consultants
Tuition assistance
Adoption assistance
Paid parental leave
Disability insurance
Life insurance
Paid time-off for vacation or illness

Applicant Tracking System Keywords

Tip: use these terms in your resume and cover letter to boost ATS matches.

Hard Skills & Tools

cycle performance modelingthermodynamic modelinguncertainty analysisengine performance testingdata correlationcomponent mappingperformance optimizationtrend analysisfuel flow analysisengine qualification

Soft Skills

technical leadershipmentoringcollaborationcommunicationdecision makingrelationship buildingindependent contributionorganizational initiative participationrisk communicationbest practices advocacy

Certifications

Bachelor's degree in engineeringAdvanced degree in Mechanical EngineeringAdvanced degree in Aerospace EngineeringU.S. Government Security Clearance