Simulation of Ice Accretion on Airfoils during Flight

2003-01-2137

06/16/2003

Event
FAA In-flight Icing / Ground De-icing International Conference & Exhibition
Authors Abstract
Content
In this study, a computational method is presented that computes ice accretion on airfoils in specified icing conditions. A good agreement is found with the ice shapes predicted by other computational methods. Agreement with the experimental ice shapes is fair. Also, the implementation and application of a mathematical model of a thermal anti-icing system in the ice accretion simulation code 2DFOIL-ICE is presented. The numerical code has proved to be able to calculate the main parameters of an airfoil anti-icing system, such as: solid surface temperatures (for the wetted region), runback water flow and convection heat transfer coefficient distributions along the external surface.
Meta TagsDetails
DOI
https://doi.org/10.4271/2003-01-2137
Pages
15
Citation
Dillingh, J., and Hoeijmakers, H., "Simulation of Ice Accretion on Airfoils during Flight," SAE Technical Paper 2003-01-2137, 2003, https://doi.org/10.4271/2003-01-2137.
Additional Details
Publisher
Published
Jun 16, 2003
Product Code
2003-01-2137
Content Type
Technical Paper
Language
English