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Turbulent spots in hypersonic transitional planar and axisymmetric boundary layers – CORRIGENDUM

Published online by Cambridge University Press:  24 June 2026

Abstract

Information

Type
Corrigendum
Copyright
© The Author(s), 2026. Published by Cambridge University Press
Figure 0

Figure 7. Normalised spot leading-edge (Small solid black square.) and trailing-edge (black dimand) speeds of turbulent spots identified in all the experiments conducted over (a) the flat plate and (b) the cone. In both the figures (dots) and (line bar) show the lower and upper bounds of the 95 % confidence interval for normalised leading-edge and trailing-edge speeds, respectively.