# Principal Engineer Applied Aerodynamics at EDGE Group

EDGE Group is hiring a Principal Engineer Applied Aerodynamics in Abu Dhabi, United Arab Emirates. Level rates it Little AI ●○○○; you can [apply on EDGE Group](https://jobsbylevel.com/go/eef57cb6-d224-43f3-bd7a-e20612de015e?utm_medium=ai-agent).

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

## Details

- Company: [EDGE Group](https://jobsbylevel.com/companies/edge-group)
- AI level: AI Level 1 (score 0 out of 100)
- Location: Abu Dhabi, Abu
- Posted: October 26, 2026
- Apply: https://jobsbylevel.com/go/eef57cb6-d224-43f3-bd7a-e20612de015e?utm_medium=ai-agent
- Free CV review for this job: https://jobsbylevel.com/cv-review?job=principal-engineer-applied-aerodynamics-at-edge-group-929d08

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## 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 The Principal Applied Aerodynamics Engineer shall demonstrate technical ownership, sound physical intuition, disciplined judgment, and accountability for the aerodynamic products assigned to the position. The engineer shall treat aerodynamic predictions as evidence with defined assumptions, uncertainty, configuration, and validity limits rather than as unquestionable numerical outputs. The engineer shall develop and maintain a mental model of the expected flow physics before reviewing computational or experimental results. RESPONSIBILITIES Develop aerodynamic concepts and configuration solutions that support aircraft-level mission and performance requirements. Evaluate candidate wing, tail, canard, fuselage, forebody, control-surface, nacelle, inlet, propulsion, and external-store arrangements. Define aerodynamic requirements and design objectives for assigned configurations or work packages. Establish appropriate aerodynamic analysis plans using analytical, empirical, computational, and experimental methods. Develop and maintain aerodynamic geometry suitable for analysis, design optimization, wind-tunnel models, and aircraft definition. Assess aerodynamic implications of outer-mold-line changes and manufacturing deviations. Conduct aerodynamic analyses using handbook, empirical, lifting-line, vortex-lattice, panel, Euler, RANS, or higher-fidelity methods as appropriate. Define CFD domains, meshes, boundary conditions, numerical schemes, turbulence models, transition assumptions, convergence requirements, and reporting criteria. Conduct mesh-sensitivity, timestep-sensitivity, domain-sensitivity, and model-sensitivity studies. Review surface pressures, flow topology, shocks, separation, wakes, vortices, and other physical evidence in addition to integrated coefficients. Develop airfoil, wing, twist, camber, thickness, spanload, and tip-shape solutions. Develop or assess high-lift systems and control-surface aerodynamic characteristics. Perform aerodynamic drag breakdowns and identify credible drag-reduction opportunities. Determine lift, drag, force, moment, stability, and control characteristics across the required flight envelope. Assess nonlinear, high-angle-of-attack, post-stall, asymmetric, and control-saturation behavior where applicable. Evaluate control effectiveness, aerodynamic balance, hinge moments, flow blanketing, and adverse aerodynamic interactions. Support wing loading, thrust-to-weight, design lift coefficient, cruise condition, takeoff, landing, maneuver, and envelope trades. Assess aerodynamic compatibility with mass properties and center-of-gravity ranges. Support propulsion integration, including inlet, nacelle, propeller, exhaust, cooling-flow, and engine-out effects. Assess the aerodynamic effects of landing gear, antennas, sensors, payloads, stores, gaps, steps, protuberances, and other installed features. Define wind-tunnel objectives, model requirements, test matrices, instrumentation, corrections, repeatability requirements, and acceptance criteria. Support wind-tunnel testing, monitor data quality, and direct changes to test priorities when evidence requires it. Reduce and interpret wind-tunnel data, including relevant tares,

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