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Numerical analysis of propeller induced ground vortices by actuator disk model
ABSTRACT: During the ground operation of aircraft, the interaction between the propulsor-induced flow field and the ground may lead to the generation of ground vortices. Utilizing numerical approaches, the source of vorticity entering ground vortices is investigated. The results show that the produc...
Autores principales: | Yang, Y., Veldhuis, L. L. M., Eitelberg, G. |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Springer Berlin Heidelberg
2017
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5758657/ https://www.ncbi.nlm.nih.gov/pubmed/29367829 http://dx.doi.org/10.1007/s12650-017-0444-4 |
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