On the unsteady throttling dynamics and scaling analysis in a typical hypersonic inlet-isolator flow

K. Raja Sekar, S. K. Karthick, S. Jegadheeswaran +1

The flow field in a two-dimensional three-ramp hypersonic mixed-compression inlet in a freestream Mach number of $M_{\infty }=5$ is numerically solved to understand the unsteady throt…