Flow over a Wing with Leading-Edge Undulations
By Alex Skillen, A. Revell, A. Pinelli, Ugo Piomelli, J. Favier. 2015
147 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/eca795fd1963169405c633d1aac2bbaa5fa2afc9
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Evolution of the streamwise vortices generated between leading edge tubercles (2016, background): “The presence of these streamwise vortices has been shown in previous work (Custodio 2007; Pedro & Kobayashi 2008; Stanway 2008; Skillen et al. 2014); however, the spanwise location of vorticity was not clear in these results and the vorticity was not quantified as it has been in this study.”
- On the reduction of aerofoil–turbulence interaction noise associated with wavy leading edges (2016, background): “…in recent years with regard to their benefits in terms of improved aerodynamic/hydrodynamic performance, particularly at high angles of attack close to the stall (Johari et al. 2007; Hansen, Kelso & Dally 2011; Yoon et al. 2011; Guerreiro & Sousa 2012; Zhang, Wang & Xu 2013; Skillen et al. 2014).”
- An experimental study on flow separation control of hydrofoils with leading-edge tubercles at low Reynolds number (2015, methodology): “Similar simulation work was also conducted by Weber et al. (2011) at Reynolds number between 5.”
- Performance and mechanism of sinusoidal leading edge serrations for the reduction of turbulence–aerofoil interaction noise (2017, background): “More recently, Skillen et al. (2014) have also explored the mechanism involved in the reduction of the separation region at high angles of attack by the use of serrated aerofoils.”