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This article is cited in 2 scientific papers (total in 2 papers)
Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$
A. D. Kosinov, M. V. Piterimova, A. V. Shmakova, N. V. Semenov, Yu. G. Ermolaev Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, Russia
Abstract:
Using the results of experimental studies, a comparison is made of the space-time distributions of the amplitude of controlled pulsations in the linear and weakly nonlinear phases of the development of a wave train in homogeneous and inhomogeneous boundary layers on a flat plate at a Mach number $\mathrm{M}=2$. (The inhomogeneity of the flow is caused by a longitudinal stationary perturbation generated by a pair of weak shock waves. Controlled perturbations were generated locally from the surface at a fixed power of the high-frequency glow discharge inside the model.) It is established that the inhomogeneity of the flow changes the mechanism of interaction of subharmonic perturbations. It is shown that in the center of the wave train there is a violation of the spatial synchronism of pulsations of subharmonic frequency.
Keywords:
supersonic flow, flat plate, boundary layer, weak shock waves, controlled disturbances.
Received: 23.11.2022 Revised: 17.02.2023 Accepted: 27.02.2023
Citation:
A. D. Kosinov, M. V. Piterimova, A. V. Shmakova, N. V. Semenov, Yu. G. Ermolaev, “Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$”, Prikl. Mekh. Tekh. Fiz., 64:4 (2023), 118–129; J. Appl. Mech. Tech. Phys., 64:4 (2023), 656–666
Linking options:
https://www.mathnet.ru/eng/pmtf1679 https://www.mathnet.ru/eng/pmtf/v64/i4/p118
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Abstract page: | 44 | References: | 16 | First page: | 8 |
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