Progress in Flight Physics 2017
DOI: 10.1051/eucass/2016090497
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Free transition on a slender cone in a quiet and a conventional wind tunnel and the effect of ultrasonically absorptive materials

Abstract: Transition from laminar to turbulent hypersonic boundary layers is the topic of several research projects world-wide. Most experimental work is done in conventional wind tunnels, although their free stream turbulence does not match free §ight conditions and has a signi¦cant in §uence onto the transition process. Experiments performed with the same 3 degree half angle cone in a conventional and a quiet wind tunnel at Mach 6 justify this approach. The formation, ampli¦cation, and decay of the second (Mack) modes… Show more

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