Improved k-ω-γ model for crossflow-induced transition prediction in hypersonic flow
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DOI: 10.1016/j.ijheatmasstransfer.2017.08.013
Abstract: Abstract Accurate prediction of boundary layer transition is extremely important for the aerodynamic and aerothermodynamic design of a hypersonic vehicle. Crossflow instability plays a crucial role in inducing transition in three-dimensional (3D) boundary layer. In… read more here.
Keywords: transition model; transition; crossflow induced; model ... See more keywords