We are pleased to share thatย LESSICEย participated in theย Spoke 6 Workshopย held in Pisa on February 18-19, 2025. Organized by Sapienza Universitร di Roma and Universitร di Pisa under theย ๐๐๐๐ ๐๐ญ๐๐ฅ๐ข๐๐ง ๐๐๐ฌ๐๐๐ซ๐๐ก ๐๐๐ง๐ญ๐๐ซ ๐จ๐ง ๐๐ข๐ ๐ก-๐๐๐ซ๐๐จ๐ซ๐ฆ๐๐ง๐๐ ๐๐จ๐ฆ๐ฉ๐ฎ๐ญ๐ข๐ง๐ , ๐๐ข๐ ๐๐๐ญ๐, ๐๐ง๐ ๐๐ฎ๐๐ง๐ญ๐ฎ๐ฆ ๐๐จ๐ฆ๐ฉ๐ฎ๐ญ๐ข๐ง๐ , this event focused on multiscale modeling and engineering applications.
During the workshop, our colleague Ubaldo Cella presented theย ๐ณ๐ฌ๐บ๐บ-๐ฐ๐ช๐ฌ: ๐ด๐๐๐๐๐๐๐๐๐ ๐ณ๐ฌ๐บ ๐บ๐๐๐๐๐๐๐๐๐ ๐๐๐ ๐๐-๐๐๐๐๐๐ ๐ฐ๐ช๐ฌ ๐๐๐๐๐๐๐๐๐ ๐๐๐๐๐๐๐๐๐๐ ๐๐๐๐๐๐๐, which was selected through cascade funding calls. This initiative aims to advance numerical simulation methodologies for in-flight ice formation on aircraft surfaces, contributing to enhanced safety through improved predictions of aerodynamic performance degradation caused by icing.
๐๐๐ฒ ๐๐ฌ๐ฉ๐๐๐ญ๐ฌ ๐จ๐ ๐๐๐๐-๐๐๐
โ๏ธ Understanding Ice Accretion:ย The formation of ice on aircraft surfaces occurs when supercooled water droplets impact the airframe, creating irregular ice layers thatย negatively affect aerodynamic performance and flight safety.
โ๏ธ Multidisciplinary Approach:ย Ice accretion is a complexย multiphysicsย andย multidisciplinaryย problem that requires:
โ๏ธ Aerodynamic flow analysis around complex geometries.
โ๏ธ Study of droplet trajectories and their impact on the aircraft surface.
โ๏ธ Thermodynamic modeling of the water layer, phase transitions, and heat transfer between ice and the aircraft structure.
โ๏ธ High-Fidelity Simulations: The project leverages high-resolution Large Eddy Simulation (LES) methods to improve the understanding and predictive capabilities of icing effects.
โ๏ธ Computational Challenges: LESS-ICE seeks to automate and enhance computational grid generation, minimizing manual intervention and improving simulation efficiency.
๐๐จ๐ง๐ฌ๐จ๐ซ๐ญ๐ข๐ฎ๐ฆ ๐๐๐ซ๐ญ๐ง๐๐ซ๐ฌ
โ๏ธ Centro Italiano Ricerche Aerospaziali โ CIRA S.c.p.A.
โ๏ธ HIT09 s.r.l.
โ๏ธ RBF Morph s.r.l.
You can read the presentation here.