Improving Ice Accretion Simulation Through the use of CFD

2011-38-0054

06/13/2011

Event
SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing
Authors Abstract
Content
In order to correctly predict an aircraft ice accretion, the ice prediction tool shall be capable of predicting the aerodynamic characteristics of both clean and iced airfoil and be able to predict the shape of the ice accreted on both wind tunnel and actual aircraft geometries. This requires the analysis tool to be able to correctly predict the local airflow on aerodynamic surfaces that have large separation regions, as well as local water impingement, freezing, convective cooling and evaporation rates. The capability of different RANS models to predict the aerodynamic degradation of an iced airfoil is evaluated. Additionally it is tested whether a more detailed simulation, that includes a more sophisticated computational model (a Navier-Stokes CFD code instead of a panel method code) which keeps the wing lift constant over the simulated time period, rather than using a constant wing angle-of-attack, would influence the resultant ice shape for a typical aircraft performing a holding, in a severe ice environment.
Meta TagsDetails
DOI
https://doi.org/10.4271/2011-38-0054
Pages
13
Citation
Silva, D., and Trapp, L., "Improving Ice Accretion Simulation Through the use of CFD," SAE Technical Paper 2011-38-0054, 2011, https://doi.org/10.4271/2011-38-0054.
Additional Details
Publisher
Published
Jun 13, 2011
Product Code
2011-38-0054
Content Type
Technical Paper
Language
English