Computational Investigations on the Effects of Gurney Flap on Airfoil Aerodynamics

The present study comprises steady state, two-dimensional computational investigations performed on NACA 0012 airfoil to analyze the effect of Gurney flap (GF) on airfoil aerodynamics using k-ε RNG turbulence model of FLUENT. Airfoil with GF is analyzed for six different heights from 0.5% to 4% of t...

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Detalles Bibliográficos
Autores principales: Jain, Shubham, Sitaram, Nekkanti, Krishnaswamy, Sriram
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2015
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4897339/
https://www.ncbi.nlm.nih.gov/pubmed/27347517
http://dx.doi.org/10.1155/2015/402358

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4897339/
https://www.ncbi.nlm.nih.gov/pubmed/27347517
http://dx.doi.org/10.1155/2015/402358

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