On the stability of supersonic boundary layer in interaction with weak shock waves
Stanislav Kirilovskiy,
Tatiana Poplavskaya,
Andrey Sidorenko
Abstract:Numerical simulation of the problem of interaction of the supersonic (M∞=2) boundary layer on the plate with weak shock waves was performed. The shock wave was generated using a wedge located above the plate. The problem was solved using the computational technology, combining the ANSYS Fluent gasdynamic package, which calculates the main flow, and the LOTRAN 3.0 software package, which calculates not only the stability of no-break flow, but also the laminar flow failure. The intensity of the incident shock wa… Show more
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