FEM analysis of in-flight ice break-up
Using a fracture mechanics framework, we present a finite element method to simulate the break-up of 2D ice accreted on the wings of aircraft and the shedding of 3D ice accreted on blades of helicopter. The fully automated ice break-up module is integrated in FENSAP-ICE [1-2], which is an in-flight...
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| Format: | Others |
| Language: | en |
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McGill University
2013
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| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=114560 |