A Methodology for the Prediction of Rotor Blade Ice Formation and Shedding

2011-38-0090

06/13/2011

Event
SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing
Authors Abstract
Content
An integrated approach for modeling the ice accretion and shedding of ice on helicopter rotors is presented. A modular framework is used that includes state of the art computational fluid dynamics, computational structural dynamics, rotor trim, ice accretion, and shedding tools. Results are presented for performance degradation due to icing, collection efficiency, surface temperature and water film properties associated with runback-refreeze phenomena, and shedding. Comparisons with other published simulations and test data are given.
Meta TagsDetails
DOI
https://doi.org/10.4271/2011-38-0090
Pages
10
Citation
Bain, J., Sankar, L., Aubert, R., and Flemming, R., "A Methodology for the Prediction of Rotor Blade Ice Formation and Shedding," SAE Technical Paper 2011-38-0090, 2011, https://doi.org/10.4271/2011-38-0090.
Additional Details
Publisher
Published
Jun 13, 2011
Product Code
2011-38-0090
Content Type
Technical Paper
Language
English