Skip to main content
. 2020 Dec 14;10:21922. doi: 10.1038/s41598-020-79048-w

Figure 5.

Figure 5

Computational domain (a), Mach contour slices and streamlines at 3D region at the leading edge (b), Mach contour corresponding to a 2D simulations (c), Mach contour cut on 2D region from 3D simulation (d) for a supersonic airfoil.