View Video Presentation: https://doi. org/10.2514/6.2022-3398. vid The AIAA 1st ice
prediction workshop focused on establishing current 2D and 3D simulation capabilities …

View Video Presentation: https://doi. org/10.2514/6.2022-3307. vid This paper presents the
Politecnico di Milano Icing Research Group's contribution to the first AIAA Ice Prediction …

Ice accretion and its aerodynamic effect on highly three-dimensional swept wings are
extremely complex phenomena important to the design, certification and safe operation of …

A comparison of computational and experimental ice accretions generated on three swept-
wing models in the NASA Glenn Icing Research Tunnel is presented. The wind tunnel …

Two-dimensional and quasi-3D in-flight ice accretion simulation codes have been widely
used by the aerospace industry for the last two decades as an aid to the certification …

MANY aircraft certified for flight in icing conditions employ anti-icing systems on wing and
empennage leading edges, as well as engine nacelles and other aerodynamic surfaces. In …

In the past two decades 2D and quasi-3D in-flight ice prediction codes have been
developed and widely used by the aerospace industry. Although efficient for calculating ice …

ASA, FAA, ONERA, the University of Illinois, Boeing and others are working on a research
program, called SUNSET2, which aims to improve our understanding and ability to model …

An effort to develop at, hree-dimcnsioi~ al ice accretioii modeling method has been initiated.
This first step t. owards creation of a complete aircraft icing simnlation code builds on …

BECAUSE not all certification conditions can be ice tunnel tested, ight tested, tank tested, or
encounteredin natural icing testing, only analytical methods make it possible to explore …