Conditional Analysis of a Shock Wave and Turbulent Boundary Layer Interaction
ORAL
Abstract
The characterization of the aperiodic cycle of unsteadiness in shock wave and turbulent boundary layer interaction (STBLI) is presented for a 24$^{\circ}$ compression ramp configuration with a fully turbulent incoming boundary layer at Mach 2.9. In previous work on the direct numerical simulation (DNS) at similar conditions, Priebe and Martín (JFM 2012) found that the aperiodic low-frequency unsteady shock motion is related to the phase of separation bubble growth and collapse. At a reduced computational cost as compared to the DNS, the large eddy simulation (LES) enables the generation of data covering a sufficiently long sampling time to converge the conditional statistics on the phases of the cycle.
*This research is supported by AFOSR Grant Number AF/9550-10-1-0164 and by the Department of Defense through the NDSEG Fellowship Program.
–