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. Author manuscript; available in PMC: 2019 Oct 19.
Published in final edited form as: Annu Rev Fluid Mech. 2018 Jan;50:535–561. doi: 10.1146/annurev-fluid-122316-045241

Figure 7.

Figure 7

(a) Surface pressure coefficients for a NACA 4412 airfoil at angle of attack (AoA) 13.8°. The dark blue line represents a dynamic slip wall model (Bose & Moin 2014); the gray hexagons represent the experiment (Wadcock 1978). (b) Surface pressure coefficients for the MD 30P/30N multi-element airfoil at AoA = 19°. The purple dashed and solid lines represent no wall model and an equilibrium wall model, respectively (Bodart & Larsson 2011); the light blue squares represent the experiment (Chin et al. 1993). Panel a reproduced from Bose & Moin (2014). Panel b reproduced from Bodart & Larsson (2011).