Analysis of Ice Release from a Rotating Propeller

2015-01-2079

06/15/2015

Event
SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures
Authors Abstract
Content
The introduction of ice-phobic coatings promises to allow passive ice protection systems to be developed particularly for rotating systems such as propellers. The centrifugal force field combined with reduced adhesive strength can produce a self-shed capability limiting the amount of ice build-up.
The size and shed time of ice shed from a propeller is predicted using a process that determines ice shape, ice growth rate and both internal and ice-structure interface stresses. A simple failure model is used to predict the onset of local failure and to propagate damage in the ice until local ice shedding is obtained.
Recommendations are made on developing the model further.
Meta TagsDetails
DOI
https://doi.org/10.4271/2015-01-2079
Pages
7
Citation
Hatch, C., Moller, J., Kalochristianakis, E., and Roberts, I., "Analysis of Ice Release from a Rotating Propeller," SAE Technical Paper 2015-01-2079, 2015, https://doi.org/10.4271/2015-01-2079.
Additional Details
Publisher
Published
Jun 15, 2015
Product Code
2015-01-2079
Content Type
Technical Paper
Language
English