State-of-the-Art Aircraft Icing and Anti-Icing Simulation
The paper gives a brief description of the various state-of-the-art mathematical models used to simulate ice accretion and anti-icing simulation on an aircraft wing section. These models are implemented in the CANICE code. CANICE results from a typical icing and anti-icing simulation are presented i...
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| Format: | article |
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2003
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| Online Access: | https://eprints.kfupm.edu.sa/id/eprint/820/1/fsaeed-2002araj.pdf |
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