Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique

ABSTRACT: In this study, the effect of cutting the end of a thick airfoil and adding a cavity on its flow pattern is studied experimentally using PIV technique. First, by cutting 30% chord length of the Riso airfoil, a thick blunt trialing-edge airfoil is generated. The velocity field around the ori...

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Detalles Bibliográficos
Autores principales: Taherian, Gholamhossein, Nili-Ahmadabadi, Mahdi, Karimi, Mohammad Hassan, Tavakoli, Mohammad Reza
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer Berlin Heidelberg 2016
Materias:
Regular Paper
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5610673/
https://www.ncbi.nlm.nih.gov/pubmed/29026342
http://dx.doi.org/10.1007/s12650-016-0405-3

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5610673/
https://www.ncbi.nlm.nih.gov/pubmed/29026342
http://dx.doi.org/10.1007/s12650-016-0405-3

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