ICE GENESIS · Creating the next generation of 3D simulation means for icing

Current design methodologies used to characterise ice accretion and its effects on air vehiclecomponents and power plant systems are mainly based on empirical methods, comparative analysis,2D simulation tools and past experience gained on in-service products. Due to the associateduncertainties, cautious design margins are used, leading to conservative and non-optimised solutions.As future air vehicle and propulsive system architectures introduce radical design changes, it willno longer be possible to rely on the existing design methodologies, making future developmentextremely difficult to accomplish efficiently and within short development cycles that are demandedby customers and desired by industry. These difficulties are increased by the recent changesin certification regulations, in particular for Supercooled Large Droplets (SLD), which requiremanufacturers to certify their products against more stringent requirements. Snow also remainsa challenge, especially for turbine engines and APUs. ICE GENESIS will provide the Europeanaeronautical industry with a validated new generation of 3D icing engineering tools (numericalsimulation tools and upgraded test capabilities), addressing App C, O and snow conditions, for safe,efficient, right first time, and cost effective design and certification of future regional, business andlarge aircraft, rotorcraft and engines. ICE GENESIS will permit weather hazards to be more preciselyevaluated and properly mitigated thanks to adapted design or optimised protection through eitheractive or passive means. Furthermore, ICE GENESIS will pave the way for 3D digital tools to be usedin the future as acceptable means of compliance by the regulation authorities. Overall, ICE GENESISwill contribute to flight safety, reduced certification costs and increased operability.