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Advances in Aerodynamics
Fig. 6 | Advances in Aerodynamics

Fig. 6

From: A symmetry-based length model for characterizing the hypersonic boundary layer transition on a slender cone at moderate incidence

Fig. 6

The Reynolds shear stress profiles at four streamwise locations for the GAC-0 case, plotted in a the inner coordinate and b the outer coordinate. Rex=3.62E6 indicates the transition onset location and Rex=6.05E6 indicates the transition peak location. Solid line denotes the DNS data of Pirozzoli et al. for an adiabatic flat-plate TBL at Ma=2.25 [31]

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