Second-Mode Transition on Flared Cone In Mach-6 Quiet Flow
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DOI: 10.2514/1.a36439
Abstract: Hypersonic boundary-layer transition was characterized on a flared cone geometry in the Boeing/AFOSR Mach-6 Quiet Tunnel. Experiments in low-disturbance, quiet flow at five unit Reynolds numbers from [Formula: see text] to [Formula: see text] measured… read more here.
Keywords: see text; mode; quiet flow; transition ... See more keywords