Analysis of unsteady behaviour in shockwave turbulent boundary layer interaction

Abstract : The unsteady behaviour in shockwave turbulent boundary layer interaction is investigated by analysing results from a large eddy simulation of a supersonic turbulent boundary layer over a compression-expansion ramp. The interaction leads to a very-low-frequency motion near the foot of the shock, with a characteristic frequency that is three orders of magnitude lower than the typical frequency of the incoming boundary layer. Wall pressure data are first analysed by means of Fourier analysis, highlighting the low-frequency phenomenon in the interaction region. Furthermore, the flow dynamics are analysed by a dynamic mode decomposition which shows the presence of a low-frequency mode associated with the pulsation of the separation bubble and accompanied by a forward-backward motion of the shock.
Complete list of metadatas

Cited literature [17 references]  Display  Hide  Download

https://hal-polytechnique.archives-ouvertes.fr/hal-00994470
Contributor : Denis Roura <>
Submitted on : Tuesday, June 3, 2014 - 9:21:16 PM
Last modification on : Wednesday, March 27, 2019 - 4:39:25 PM
Long-term archiving on : Wednesday, September 3, 2014 - 10:50:38 AM

File

S0022112012000377a.pdf
Publisher files allowed on an open archive

Identifiers

Collections

Citation

Muzio Grilli, Peter J. Schmid, Stefan Hickel, Nikolaus A. Adams. Analysis of unsteady behaviour in shockwave turbulent boundary layer interaction. Journal of Fluid Mechanics, Cambridge University Press (CUP), 2012, 700, pp.16-28. ⟨10.1017/jfm.2012.37⟩. ⟨hal-00994470⟩

Share

Metrics

Record views

634

Files downloads

961