On the influence of a single roughness element on the flow in supersonic boundary layer on a blunted cone


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The work presents the results of numerical modeling of a supersonic flow around a blunted cone with an isolated cylindrical roughness on the forebody surface in the three-dimensional formulation. The roughness element is shown to distort the mean flow and to give rise to small-amplitude disturbances with distinguished spectral peaks in the boundary layer.

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S. Kirilovskiy

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

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Email: kirilov@itam.nsc.ru
俄罗斯联邦, Novosibirsk; Novosibirsk

T. Poplavskaya

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Email: kirilov@itam.nsc.ru
俄罗斯联邦, Novosibirsk; Novosibirsk

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