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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...
Autores principales: | , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Springer Berlin Heidelberg
2016
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Materias: | |
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 |