Ice Crystal Accretion Tool (ICAT) capabilities on heated NACA0012 Airfoil

2023-01-1388

06/15/2023

Features
Event
International Conference on Icing of Aircraft, Engines, and Structures
Authors Abstract
Content
The present paper showcases the predicting ability of an in-house 2D/ Quasi-3D steady state Ice Crystal Accretion Tool (ICAT) applicable for both heated and un-heated surfaces. The previously existing code for unheated surfaces, has been extended to heated scenarios with the inclusion of: 1) coupling with solid conduction model 2) inclusion of advanced models for crystal melting, water film modeling, sticking and erosion. The results obtained from ICAT are verified against the experimental results of heated NACA0012 airfoil, conducted in the icing wind tunnel of TU Braunschweig as part of MUSIC-haic project. ICAT predictions are found to be well in agreement with the ICI physics, which is proven with the various parameters addressed in this paper, such as tunnel temperature, ice crystal temperature, inlet melt ratio, heating power, etc.
Meta TagsDetails
DOI
https://doi.org/10.4271/2023-01-1388
Pages
6
Citation
Roychowdhury, S., Poornima, R., Bokade, V., Jebauer, S. et al., "Ice Crystal Accretion Tool (ICAT) capabilities on heated NACA0012 Airfoil," SAE Technical Paper 2023-01-1388, 2023, https://doi.org/10.4271/2023-01-1388.
Additional Details
Publisher
Published
Jun 15, 2023
Product Code
2023-01-1388
Content Type
Technical Paper
Language
English