On low-frequency unsteadiness in three-dimensional shock/boundary layer interactions
ORAL
Abstract
We carry out DNS of shock/boundary layer interactions (SBLI) in the presence of cross flow, as a surrogate of genuine three-dimensional SBLI. Use of spanwise wide computational domains suggests the presence of organized, large-scale rippling of the instantaneous flow separation line, on a typical length scale proportional to the mean separation extent. We present evidence that In the presence of cross flow these ripples are advected at a fraction of the mean spanwise velocity. Based on the observed data we obtain a predictive formula for the typical frequency of the large-scale unsteadiness, which very well conforms with the computed frequency spectra. In agreement with what observed in experiments and DNS of three-dimensional SBLI, the typical frequency is predicted to increase with the flow skew angle.
*This work was supported by TEAMAero Horizon 2020 research and innovation program under grant agreement 860909 and by the Air Force Office of Scientific Research under grants FA9550-19-1-0210 and FA9550-19-1-7029.We acknowledge that the results reported in this paper have been achieved with computational resources of IscrB\_THIPHRE and IscrB\_3dSBLI projects, using the PRACE Research Infrastructure resource MARCONI100 based at CINECA, Casalecchio di Reno, Italy.
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Presenters
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Alessandro Ceci
- Sapienza University of Rome