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Start of the LOM-Ice Project
Certification Specifications. Icing wind tunnel tests represent one of the most important means of compliance in this respect. Icing and snow conditions are generated in icing wind tunnels by injecting water particles [...] in wind tunnels. A measurement technique that is both non-intrusive, capable of sampling wide spatial regions, and measuring a large set of cloud features, will be provided as a support for wind tunnel [...] monitoring of the injected particle clouds. This is especially important for snow conditions, for which wind tunnel cloud generation technologies are still under development. In this perspective, it is crucial
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LOM-Ice
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/lom-ice
Certification Specifications. Icing wind tunnel tests represent one of the most important means of compliance in this respect. Icing and snow conditions are generated in icing wind tunnels by injecting water particles [...] in wind tunnels. A measurement technique that is both non-intrusive, capable of sampling wide spatial regions, and measuring a large set of cloud features, will be provided as a support for wind tunnel [...] Development of a Laser Optical Measurement technique for the characterization of particle clouds in Icing wind tunnels © RTA Proving aircraft safe operation in icing and snow conditions is required by the European
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JOICE
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/joice
aircraft in-flight icing. The technical activities in JOICE comprise the following: Advancement of icing wind tunnel infrastructure Execution of experiments in simulated icing conditions Numerical simulation [...] be used for high-accuracy measurements of ice-induced aerodynamic effects in ordinary aerodynamic wind tunnels AIT focuses on the development of snow simulation models and tools and on extending the current
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IMPACT
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/impact
The project will also optimize its aerostructural properties and validate the technology with Icing Wind Tunnel tests. The four main objectives of IMPACT are: unlocking the capability to perform fast and [...] simulations and the performance of passive anti-ice coating and devices by means of large scale icing wind tunnel (IWT) experimental tests. Facts IMPACT – Aircraft advanced rear end and empennage optimisation
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EREA Young Researchers Event at AIT
by laboratory tours at the AIT (including Battery Lab and Drive Lab) and a visit to the RTA Climate-Wind-Channel. A social dinner was also not to be missed to make contacts and network with other organisations
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InSPIRe – innovative aircraft ice protection
Ice on Regional Aircraft, has held its kick-off meeting together with colleagues from the CIRA Icing Wind Tunnel facility at Leonardo’s Aircraft Division in Pomigliano d’Arco, Naples, Italy on March 7th and
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ICE GENESIS
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/ice-genesis
icing wind tunnels to allow reproduction of: Supercooled Large Droplets (SLD) in FZDZ (Freezing drizzle) conditions. Snow icing conditions Additionally, to assess the potential of current icing wind tunnels
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SNOWING
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/snowing
industry is facing increasing needs for snow testing in reliable and re-producible conditions (e.g. icing wind tunnels, IWT) and for validated numerical tools to sup-port product development and certification
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No-Ice-Rotor
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/no-ice-rotor
Validate the ice protection system performance by testing the demonstrator in a large scale Icing Wind Tunnel Facts NO-ICE-ROTOR - Development and demonstration of materials and manufacturing process for
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TRIcEPS
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/triceps
The full system will be tested and qualified through extensive testing, which will include Icing wind tunnel measurements and structural tests. TRIcEPS will deliver the air intake, its engine protection
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InSPIRe
- /en/research-topics/hybrid-electric-aircraft-technologies/projects/inspire
integrated into the LE composite structure. Performance verification are pursued by means of an Icing Wind Tunnel (IWT) test campaign to contribute to reaching TRL5 for the selected IPS technologies. Facts
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