The formation mechanism and impact of streamwise vortices on NACA 0021 airfoil's performance with undulating leading edge modification

By N. Rostamzadeh, K. Hansen, R. Kelso, B. Dally. 2014

136 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/239413d7c910b25e48c088a8e617df8ea910212c

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In Aerospace Engineering

1. N. Rostamzadeh
2. R. Kelso
3. K. Hansen
4. B. Dally

In Computational Mechanics

1. N. Rostamzadeh
2. R. Kelso
3. K. Hansen
4. B. Dally

Citations in the corpus

• Evolution of the streamwise vortices generated between leading edge tubercles (2016, background): “This mechanism is activated by the presence of skewness in the flow, arising from spanwise pressure gradients, and vorticity within the boundary layer (Rostamzadeh et al. 2014).”