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3. Example of Second-Mode Instability Dominance at a Mach Number of 5.2
4. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
5. 5Rufer,S.J.,andSchneider,S.P."Hot-WireMeasurementsofInstabilityWavesonConesatMach6,"AIAA Paper2006-3054,June2006.