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In your role as a Performance Engineer, you will be responsible for analyzing, modeling, and optimizing aircraft and propulsion system performance across the full flight envelope. This position requires strong expertise in gas turbine engine cycles, aerodynamics, and thermodynamics to support aircraft development, certification, and operational excellence.
Job Responsibility:
Perform thermodynamic cycle analysis of turbofan engines, evaluating thrust, TSFC, efficiency, operability margins, and performance across the flight envelope
Develop, validate, and maintain propulsion system performance models to support aircraft integration, certification, and customer deliverables
Generate aircraft and engine performance data for flight manuals, flight computers, and executive-level program assessments
Conduct runway and mission performance analyses
Support engine-airframe integration efforts, including takeoff thrust optimization and safety-focused performance methodologies
Author and execute flight test plans to evaluate propulsion robustness, operability, and early design maturity
Contribute to advanced combustion and fluid dynamics modeling efforts
Support experimental testing efforts including aeroacoustics, flow visualization (Schlieren), wind tunnel testing, and telemetry data analysis
Play a key role within our HEAT (High-Enthalpy Airflow Test) facility, including sizing, analyzing, and optimizing this world-class test infrastructure
Requirements:
Bachelor’s degree in Aerospace Engineering, Mechanical Engineering, or related field
Strong foundation in thermodynamics, compressible flow, gas turbine engine cycles, and aerodynamics
Experience with propulsion performance modeling and aircraft performance analysis
Proficiency in MATLAB and Python
Demonstrated ability to interpret and validate complex engineering data sets
Strong systems-level thinking with attention to both detailed analysis and program-level impacts
Demonstrated leadership in technical initiatives or cross-functional collaboration
Nice to have:
Master’s degree in Aerospace Engineering with focus on propulsion, aerothermodynamics, or combustion
Experience supporting turbofan engine development programs
Background in CFD, Large Eddy Simulation (LES), or reduced-order modeling techniques
Exposure to experimental aerodynamics, aeroacoustics, or high-speed flow diagnostics