Published January 25, 2023 | Version v1
Journal article Open

On low-frequency unsteadiness in swept shock wave–boundary layer interactions

  • 1. Sapienza University of Rome
  • 2. University of Maryland

Description

We derive a scaling law for the characteristic frequencies of wall pressure fluctuations
in swept shock wave/turbulent boundary layer interactions in the presence of cylindrical
symmetry, based on analysis of a direct numerical simulations database. Direct numerical
simulations in large domains show evidence of spanwise rippling of the separation line,
with typical wavelength proportional to separation bubble size. Pressure disturbances
around the separation line are shown to be convected at a phase speed proportional
to the cross-flow velocity. This information is leveraged to derive a simple model for
low-frequency unsteadiness, which extends previous two-dimensional models (Piponniau
et al., J. Fluid Mech., vol. 629, 2009, pp. 87–108), and which correctly predicts growth of
the typical frequency with the sweep angle. Inferences regarding the typical frequencies in
more general swept shock wave/turbulent boundary layer interactions are also discussed.

Files

on-low-frequency-unsteadiness-in-swept-shock-wave-boundary-layer-interactions.pdf

Additional details

Funding

European Commission
TEAMAero - Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications 860909