On the mechanisms of interaction of controlled disturbances in the longitudinal wake region in a supersonic boundary layer on a flat plate
The present study is aimed at searching for mechanisms of wave interaction in a supersonic boundary layer on a flat plate with the flow being distorted by a streamwise disturbance generated on a sharp leading edge by a pair of weak shock waves. The space and time distributions and the frequency-wave spectra of oscillations and their wave characteristics in the linear and weakly nonlinear phases of wave train development in a nonhomogeneous boundary layer under conditions of a fixed power of the local source of controlled disturbances are analyzed. Based on experimental results, possible variants of wave interaction in a supersonic boundary layer on a flat plate in the region of the longitudinal wake generated by an N-wave are proposed.
Authors
- Н. В. Семёнов (ORCID: https://orcid.org/0000-0003-3035-8479)
- А. Д. Косинов (ORCID: https://orcid.org/0000-0002-8626-4669)
- A. V. Shmakova
- Б. В. Смородский
- A. A. Yatskikh (ORCID: https://orcid.org/0000-0002-0217-0236)
- M. V. Piterimova
- Yu. G. Yermolaev
Institutions
- Institute of Theoretical and Applied Mechanics (RU)
Publication Details
- Journal
- Thermophysics and Aeromechanics
- Published
- 2024-10-17
- DOI
- https://doi.org/10.1134/s0869864324020021
- Citations
- 1
- Primary Topic
- Fluid Dynamics and Turbulent Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.37