Novel Methods for Rotorcraft Engine Propulsion Integration

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This PhD project aims to deliver modelling capability for the prediction of installed engine performance characteristics, throughout the design and service-life of rotorcraft. This will be accomplished with the development of a novel approach able to predict the aerodynamic performance of installed rotorcraft engines rapidly. This framework will encompass a novel method for the parametric geometry definition of rotorcraft engine components such as intakes, ducts, and exhausts. The devised method will couple with state-of-the-art tools for helicopter comprehensive analysis, Computational Fluid Dynamics (CFD), data analytics, reduced-order modelling, and Multi-Objective Optimisation (MOO).