Modeling of Supercooled Large Droplet Physics in Aircraft Icing
This paper aims to investigate phenomena that are related to SLD conditions in aircraft icing including gravity, non-spherical droplets, droplet breakup and droplet splash using an in-house computational tool. The in-house computational tool involves four modules for the computation of the flow fiel...
| Hauptverfasser: | , |
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| Format: | Artikel |
| Sprache: | English |
| Veröffentlicht: |
MDPI AG
2024-09-01
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| Schriftenreihe: | Aerospace |
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| Online Zugang: | https://www.mdpi.com/2226-4310/11/10/797 |