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An Ice Shedding Model for Rotating Components
ISSN: 0148-7191, e-ISSN: 2688-3627
Published June 10, 2019 by SAE International in United States
This content contains downloadable datasetsAnnotation ability available
A CFD simulation methodology is presented to evaluate the ice that sheds from rotating components. The shedding detection is handled by coupling the ice accretion and stress analysis solvers to periodically check for the propagation of crack fronts and possible detachment. A novel approach for crack propagation is highlighted where no change in mesh topology is required. The entire computation from flow to impingement, ice accretion and crack analysis only requires a single mesh. The accretion and stress module are validated individually with published data. The analysis is extended to demonstrate potential shedding scenarios on three complex industrially-relevant 3D cases: a helicopter blade, an engine fan blade and a turboprop propeller. The largest shed fragment will be analyzed in the context of FOD damage to neighboring aircraft/component surfaces.
|Technical Paper||Multi-Shot Icing Simulations with Automatic Re-Meshing|
|Technical Paper||CFD Analysis of Supercooled Large Droplets in Turbofan Engines|
|Technical Paper||Additional Considerations for Analytical Modeling of Rotor Blade Ice|
CitationNilamdeen, S., Zhang, Y., Ozcer, I., and Baruzzi, G., "An Ice Shedding Model for Rotating Components," SAE Technical Paper 2019-01-2003, 2019, https://doi.org/10.4271/2019-01-2003.
Data Sets - Support Documents
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