New generation of 3D icing engineering tools for liquid and snow conditions
Future air vehicle and propulsive systems architectures imply new methodologies to characterise ice accretion and its effects. Furthermore, changes in certification regulations, in particular for Supercooled Large Droplets (SDL), will require manufacturers to certify their products against more stringent requirements. Snow remains a challenge for turbine engines and APUs. The goal of the EU-funded ICE GENESIS project is to provide the European aeronautical industry with a validated new generation of 3D icing engineering tools (Icing Wind Tunnel capabilities and numerical simulation to predict ice accretion), as addressed by Appendix C, Appendix O, and snow conditions in the Federal Aviation Administration Advisory Circular for safe, efficient and cost effective design and certification of future aircraft and rotorcraft.
Call for proposal
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Funding SchemeRIA - Research and Innovation action
60313 Frankfurt Am Main
H3T 1J4 Montreal
H3B 1Y8 Montreal