Author:
Breitfuß Wolfgang,Ferschitz Hermann,Schwarzenboeck Alfons,Heller Romy,Pervier Hugo,Dupuy Regis,Jaffeux Louis,Berne Alexis
Abstract
<div class="section abstract"><div class="htmlview paragraph">The simulation of natural-like snow conditions in a controlled environment such as an Icing Wind Tunnel (IWT) is a key component for safe, efficient and cost-effective design and certification of future aircraft and rotorcraft. Current capabilities do not sufficiently match the properties of natural snow, especially in terms of size and morphology. Within the Horizon 2020 project ICE GENESIS, a new technology has been developed aiming to better recreate natural snowflakes. The focus of the newly developed system was the generation of falling snow in a temperature range of +1°C to -4°C. Ground measurements and flight test campaigns have been performed to better characterize these conditions and provide requirements for wind tunnel facilities. The calibration results of the new snow generation system as well as snow accretion data on a NACA0012 test article with a chord length of 0.377 m are presented. The influence of different snow conditions on the accretion rate and the overall shape were investigated, revealing significant differences for different snow qualities.</div></div>
Reference11 articles.
1. Baumert , A. , Bansmer , S. , and Bacher , M. Implementation of an Innovative Ice Crystal Generation and Conveyance System to the Icing Wind Tunnel Braunschweig 53rd AIAA Aerospace Sciences Meeting and Exhibit 2015
2. Currie , T.C. , Struk , P.M. , Tsao , J.-C. Fuleki , D. et al. Fundamental Study of Mixed-phase Icing with Application to Ice Crystal Accretion in Aircraft Jet Engines 4th AIAA Atmoshperic and Space Environments Conference 2012
3. Struk , P.M. , Tsao , J.-C. , and Fuleki , D.
4. European Union Aviation Safety Agency 2023
5. Federal Aviation Administration (FAA) 2014
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献