Synchronization of second-mode instability waves for high-enthalpy hypersonic boundary layers

Leonardo C. Salemi, Hermann F Fasel

Research output: Contribution to journalArticle

2 Scopus citations

Abstract

The stability of a hypersonic boundary layer for 5° half-angle cone at the Caltech T5 high-enthalpy flow conditions was investigated using direct numerical simulations. For the 'linear' stability investigations, the boundary layer was perturbed by small axisymmetric disturbances with very small amplitudes, and for the nonlinear regime, three-dimensional pulse disturbances with larger amplitudes were introduced. The surprising result from these investigations was that the 3D wave packet undergoes strong spatial modulations, which we have not observed for other experimental conditions (e.g. the Purdue BAM6QT). This modulation was found to be directly due to the synchronization between second-mode wave components and vorticity/entropy modes. Furthermore, it was found that a synchronization with slow acoustic waves leads to a sudden and strong emission of acoustic waves deep into the free stream, which was observed for both a linear wave train and a 3D nonlinear wave packet. Therefore, it can be concluded that this is a linear mechanism that is not suppressed by nonlinear effects.

Original languageEnglish (US)
Pages (from-to)R21-R214
JournalJournal of Fluid Mechanics
Volume838
DOIs
StatePublished - Mar 10 2018

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Keywords

  • boundary layer stability
  • compressible boundary layers
  • high-speed flow

ASJC Scopus subject areas

  • Condensed Matter Physics
  • Mechanics of Materials
  • Mechanical Engineering

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