Development of a Shed-Ice Trajectory Simulation in FENSAP-ICE

2007-01-3360

09/24/2007

Event
2007 SAE Aircraft and Engine Icing International Conference
Authors Abstract
Content
A numerical approach to the trajectory simulation of break-up ice in the in-flight icing code FENSAP-ICE is investigated. At each time step, the displacement and rotation of the moving domains is computed from a 6-DOFs analysis of the forces and moments. The moving domains are amalgamated into the fixed background mesh by a hole-cutting and stitching algorithm, producing a continuous unstructured hybrid mesh, eliminating interpolation between domains and ensuring that the fluxes are fully conserved across the entire mesh. To maintain good load balancing on parallel computers, the finite element CFD flow solver uses an efficient parallel iterative matrix solver and domain decomposition to partition the computational domain into equal-sized subdomains. Test cases used to validate and demonstrate the features of the computational algorithm are shown.
Meta TagsDetails
DOI
https://doi.org/10.4271/2007-01-3360
Pages
13
Citation
Baruzzi, G., Lagacé, P., Aubé, M., and Habashi, W., "Development of a Shed-Ice Trajectory Simulation in FENSAP-ICE," SAE Technical Paper 2007-01-3360, 2007, https://doi.org/10.4271/2007-01-3360.
Additional Details
Publisher
Published
Sep 24, 2007
Product Code
2007-01-3360
Content Type
Technical Paper
Language
English