# Combustion Design Senior Engineer at EDGE Group

EDGE Group is hiring a Combustion Design Senior Engineer in Abu Dhabi, United Arab Emirates. Level rates it Little AI ●○○○; you can [apply on Level](https://jobsbylevel.com/go/47bdcf23-a606-41d1-ba8d-13df9853f5c6).

AI Level 1, AI centrality 0 out of 100. Abu Dhabi.

## Details

- Company: [EDGE Group](https://jobsbylevel.com/companies/edge-group)
- AI level: AI Level 1 (score 0 out of 100)
- Location: Abu Dhabi
- Posted: October 12, 2026
- Apply: https://jobsbylevel.com/go/47bdcf23-a606-41d1-ba8d-13df9853f5c6

## Description

ABOUT EDGE At EDGE bold ideas are engineered into technologies that protect, improve and save lives. Headquartered in the United Arab Emirates, EDGE is a leading advanced technology group working at the forefront of defence and emerging technologies. Spanning more than 35 specialised companies and multiple centres of excellence, we are purpose-built to move fast. Free from heavy legacy processes, we give our people the autonomy, accountability, and agility to bring breakthrough technologies from concept to reality. Based in Abu Dhabi, a globally connected hub at the crossroads of Europe, Asia, Africa, and the Middle East, EDGE is home to a truly multicultural community where bold ideas thrive, and the future is shaped. Together, we are shaping the future. ABOUT THE ROLE Job Overview: The Gas Turbine Combustor Engineer is responsible for the design, analysis, development, and support of combustor systems for micro jet engines. The role requires the incumbent to gather and interpret customer requirements and contextualise the performance criteria in conjunction with the engine performance analysis team. It is expected that the combustor designer will use the appropriate tools for the given stage of the design process, for instance, comprehensive 1-D and correlation-based modelling for the introductory sizing phases and eventually exploit high-fidelity CFD analysis to model the complex combustion processes. The role of the designer focuses on achieving stable combustion, high efficiency, low emissions, reliable ignition, and long life within the constraints of very small engine architectures, where combustor residence time, temperature patterns, and manufacturability are especially challenging. The designer must communicate across a wide range of functions, such as system engineering, mechanical design, materials engineering, and advanced additive manufacturing, for instance. In summary, the goal of the combustor designer is to assess requirements, demonstrate innovation in the application of the tools, maintain a pragmatic product-centric outlook, and finally deliver a fit-for-purpose design. RESPONSIBILITIES Define combustor requirements from engine cycle conditions, including thrust class, allowable pressure loss, operability range, emissions intent, and turbine inlet temperature constraints. Translate system requirements into a combustor concept by selecting the overall architecture, primary zone arrangement, fuel injection approach, dilution strategy, and cooling philosophy. Carry out preliminary sizing and concept development using first-principles methods, empirical correlations, and iterative trade studies to establish feasible geometry and performance. Analyse flow field, mixing, ignition, flame stability, liner heat load, and exit temperature distribution to refine the design through successive development stages. Evaluate design sensitivities to geometry, fuel scheduling, airflow split, and manufacturing tolerance to improve robustness and reduce risk early in the process. Develop and review detailed combustor hardware, including dome, swirler, liner, dilution holes, cooling features, igniter location, and sealing interfaces. Support CFD, rig testing, and engine testing to validate assumptions, correlate analytical predictions with measured data, and update the design accordingly. Iterate the combustor design through concept, preliminary, detailed, and verification phases until performance, durability, and operability targets are met. Work closely with performance, aerodynamics, mechanical design, materials, manufacturing, and test teams to ensure the combustor design integrates cleanly into the full engine system. Document design rationale, trade-offs, test findings, and verification evidence to support technical reviews and development gates. BASIC QUALIFICATIONS Masters’s degree in Aerospace Engineering, Mechanical Engineering, Thermal Engineering, or a closely related discipline. 8–10 years of progressively

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Source: https://jobsbylevel.com/jobs/combustion-design-senior-engineer-at-edge-group-c17b8a

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