Supercooled large droplet icing and hot-air anti-icing performance of a two-dimensional nacelle lip in a large-scale icing wind tunnel
Year: 2026
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0315631
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W7130374085
