Principal Investigator:
Julien Bodart
, ISAE-SUPAERO, Université de Toulouse (France)
HPC Platform used:
JUQUEEN of JSC
Local Project ID:
PRA097
In this study, researchers in fluid mechanics at ISAE-SUPAERO investigate possible control of shock boundary layer interaction, a well known flow phenomenon occuring on high speed supersonic devices. In particular, low frequency modes have a significant impact on the device load. High fidelity simulations of turbulent flows are performed to understand the modifications of the flow field induced by the microramp vortex generators located upstream the interaction.
