\begin{document}$ {\Delta _x} = {\Delta _y} = {\lambda _y}/128 $\end{document}. A periodic boundary condition is used in the y-direction, while an outflow boundary condition is used in the x-direction. The interaction between shock and density perturbation will deposit vorticity in the density perturbation region. The width of the density perturbation region can be represented by the width of the vortex pair. The growth rate of the RM-like instability can be represented by the growth rate of the width of the density-disturbed region or the maximum perturbation velocity in the y-direction. The simulation results show that the growth rate of the vortex pair width is proportional to the perturbation wave number ky, the perturbation amplitude η, and the velocity difference before and after the shock wave Δu, specifically, δvkyΔ. In the problem of coupling the RM-like instability with the interface, we calculate the derivation of the interface perturbation amplitude with respect to time to obtain the growth rate of the interface. It is concluded from the simulations that the coupling of the RM-like instability with the interface has two mechanisms: acoustic coupling and vortex merging. When the density perturbation region is far from the interface, only acoustic wave is coupled with the interface. The dimensionless growth rate of interface perturbation caused by acoustic coupling decays exponentially with kyL, δvi/(kyΔ)∝\begin{document}$ {{\text{e}}^{ - {k_y}L}} $\end{document}. When the density perturbation region is closer to the interface, acoustic coupling and vortex merging work together. The vortex merging leads to an increase in the perturbation velocity when the Atwood number of the interface is positive. When the Atwood number is positive, reducing the Atwood number at the interface and increasing the width of the transition layer at the interface can both reduce the growth of interface perturbation caused by the RM-like instability coupling."> - 必威体育下载

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Sun Bei-Bei, Ye Wen-Hua, Zhang Wei-Yan
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  • Abstract views:2079
  • PDF Downloads:57
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Publishing process
  • Received Date:02 June 2023
  • Accepted Date:18 August 2023
  • Available Online:19 August 2023
  • Published Online:05 October 2023

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