Influence of blunt-cone tip temperature on the laminar-turbulent transition in hypersonic boundary layers
D.A. Bountin, Yu.V. Gromyko, S.V. Kirilovskiy b, A.A. Maslov a, and T.V. Poplavskaya c
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
E-mail: maslov@itam.nsc.ru a, kirilov@itam.nsc.ru b, popla@itam.nsc.ru c
Keywords: hypersonic flow, stability, heat fluxes, laminar-turbulent transition, blunt cones, local heating/cooling, Transition SST model
Pages: 483–496
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