Working paper Open Access
Bayona-Roa, Camilo;
Reyes Sotomayor, Ricardo;
García-Navarro, Juan Guillermo;
Castañeda Vergara, David;
Aljure Rey, Mauricio
This article demonstrates the conception of numerical techniques for simulating the flow around a NACA 0012 airfoil oscillating at its quarter-chord point. These simulations solve the physics of the dynamic stall phenomenon on an oscillating airfoil case. To do so, a two-dimensional framework is used to achieve feasible aerodynamic predictions. The simulations are required to test aerodynamic coefficients, corresponding to PIV (particle imaging velocimetry) images acquired experimentally according to the literature. A qualitative and quantitative agreement is expected between the simulation and the experimental results for both cases.
Name | Size | |
---|---|---|
SoPhic_Artículo1 - FSI aerodinámica actuador.zip
md5:67447ee85efb0de96648707bfe28c1a0 |
2.6 MB | Download |
All versions | This version | |
---|---|---|
Views | 47 | 47 |
Downloads | 2 | 2 |
Data volume | 5.2 MB | 5.2 MB |
Unique views | 42 | 42 |
Unique downloads | 2 | 2 |