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...

Descripción completa

Detalles Bibliográficos
Autores principales: Yang, Y., Veldhuis, L. L. M., Eitelberg, G.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer Berlin Heidelberg 2017
Materias:
Regular Paper
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

Internet

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

Ejemplares similares