
- Bachelor’s or Master’s in Mechanical or Aeronautical Engineering. Other qualifications, in combination with relevant experience, may also be considered.
- Strong technical knowledge in gas turbine performance and thermodynamic methodologies
- Understanding of cross-discipline engineering concepts which include but are not limited to system design, aerothermal, thermo-fluids, controls and aircraft performance.
- Knowledge of C++, NPSS, Matlab and Python would be beneficial.
- Highly numerate with strong technical and analytical skills, problem-solving ability and capable of systems-level thinking.
- Excellent communication and interpersonal skills, and will need to be able to contribute effectively in a team environment.
- Engine performance prediction utilising modeling skills to define/optimize propulsion systems.
- Act as whole engine integrators of propulsion system functional design, this is achieved by:
- Gathering sub-system predictions of component behavior for integration into system-level predictions.
- Negotiating sub-system performance levels to achieve optimum propulsion system level requirements.
- Develop and maintain a functional understanding of the propulsion system e.g. compressor stability, combustion stability, control system requirements & behavior.
- Understand the root cause of problems and to work with stakeholders to formulate and incorporate solutions in line with corporate guidelines.
- Engine performance verification including engine test analysis and support.
- Demonstrate an ability to continuously improve understanding and practices and share within the business
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