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Heat and Mass Transfer and Physical Gasdynamics
Numerical simulation of the interaction of a Mach wave and a boundary layer on a flat plate
I. V. Egorovab, N. K. Nguyena, N. V. Pal'chekovskayaab a Moscow Institute of Physics and Technology (National Research University), Dolgoprudny, Moscow Region
b Central Aerohydrodynamic Institute
Abstract:
Using direct numerical simulation, a problem of the interaction of a Mach wave with a boundary layer on a flat plate, streamlined by a supersonic perfect gas flow at the Mach number $\rm M = 2.5$ is considered. The influence of the intensity of the incident Mach wave on the laminar-turbulent transition (LTT) is studied. It is shown that the incidence of a Mach wave with an amplitude of $5\%$, simulating the relative thickness of the roughness on the side wall of the wind tunnel, on the boundary layer leads to the formation of a turbulent wedge in the boundary layer on a flat plate.
Received: 20.03.2023 Revised: 30.06.2023 Accepted: 03.10.2023
Citation:
I. V. Egorov, N. K. Nguyen, N. V. Pal'chekovskaya, “Numerical simulation of the interaction of a Mach wave and a boundary layer on a flat plate”, TVT, 61:5 (2023), 752–759; High Temperature, 61:5 (2023), 689–696
Linking options:
https://www.mathnet.ru/eng/tvt11863 https://www.mathnet.ru/eng/tvt/v61/i5/p752
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