Pasha, A. A., Juhany, K. A., & Khalid, M. (2018) Numerical prediction of shock/boundary-layer interactions at high Mach numbers using amodified Spalart– Allmaras model. Engineering Applications of Computational Fluid Mechanics, 12(1), 459–472. doi: 10.1080/19942060.2018.1451389
Since publication of the above article we have been notified by the Author that Figure captions 8 and 9 have been swapped in the published version.
These have now been corrected in the online version as given below:
Figure 8. Case-3: computed wall pressure (a) and skin-friction coefficient (b) using the standard SA model (Spalart & Allmaras, 1992) and the shock-unsteadiness modified SA model (Sinha et al., 2005), compared to the experiments of Holden et al. (2014) at Mach 6.
Figure 9. Case-4: computed normalized density contours using the shock-unsteadiness modified SA model (Sinha et al., 2005) (a) compared to the Schlieren image of Holden et al. (2014) at Mach 5 (b).