Numerical study of airfoil with wavy leading edge at high Reynolds number regime

In this work, a numerical study of flow around an airfoil with wavy leading edge is presented at a Reynolds number of 3X106. The flow is resolved by considering the RANS (Reynolds Average Navier-Stokes) equations. The baseline geometry is based on the NACA 0021 profile. The wavy leading edge has an...

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Vydáno v:Revista Facultad de Ingeniería Universidad de Antioquia
Hlavní autoři: William Denner Pires Fonseca, Rafael Rosário da Silva, Reinaldo Marcondes Orselli, Adson Agrico de Paula, Ricardo Galdino da Silva
Médium: Artigo
Jazyk:Inglês
Vydáno: Universidad de Antioquia 2021
Témata:
Ingeniería
CFD analysis
RANS simulation
Wavy leading edge airfoil
On-line přístup:https://www.redalyc.org/articulo.oa?id=43067842006
https://www.redalyc.org/journal/430/43067842006/
https://www.redalyc.org/journal/430/43067842006/html/
https://www.redalyc.org/journal/430/43067842006/43067842006.epub
https://www.redalyc.org/journal/430/43067842006/movil
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