Coherent structures in an airfoil boundary layer and wake at low Reynolds numbers

By S. Yarusevych, Pierre E. Sullivan, J. Kawall. 2006

153 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/0504cdc5a0e16295f70ede554b394b4ced2341f3

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In Aerospace Engineering

1. S. Yarusevych
2. Rye M. Waldman
3. A. Carrere
4. O. Curet
5. Pierre E. Sullivan
6. J. Kawall
7. K. Breuer

In Computational Mechanics

1. S. Yarusevych
2. Pierre E. Sullivan
3. J. Kawall
4. Rye M. Waldman
5. A. Carrere
6. K. Breuer
7. O. Curet

Citations in the corpus

• On vortex shedding from an airfoil in low-Reynolds-number flows (2009, methodology): “The numerical results of Lin & Pauley (1996), supported by the experimental results and stability analysis of Yarusevych et al. (2006), suggest that coherent structures can form in the separated shear layer and are attributed to the Kelvin–Helmholtz instability (cf. Watmuff 1999).”
• Aerodynamic Characterization of a Wing Membrane with Variable Compliance (2014, background): “The fundamental frequency of shedding vortices behind an airfoil has been shown to have a power-law relationship with the Reynolds number in the form of fo ∼ Re, where fo is the fundamental frequency of the flow structure, and n is the power dependency [32].”