Fantastic, pun intended. It looks like the expansion fan that is generated by the trailing edge of the separation bubble accelerates airflow which re-energizes the boundary layer.
As flight mach number goes to high or infinity the post shock density tends to high that reduces the volume of shock layer after that the shock layer will interact the boundary layer
Thank you.
Fantastic, pun intended. It looks like the expansion fan that is generated by the trailing edge of the separation bubble accelerates airflow which re-energizes the boundary layer.
thank you, sir, I had so much doubt about this topic now it's clear
As flight mach number goes to high or infinity the post shock density tends to high that reduces the volume of shock layer after that the shock layer will interact the boundary layer
thank you sir