A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow
instability known as 'buzz', characterized by unsteady shock oscillations at the inlet. This …

Experimental, numerical and theoretical investigations are carried out to grasp the effect of
angle of attack (AoA) on the performance of the supersonic intake for High-Mach Integrated …

The main goal of today's car designers is to minimize fuel consumption in all possible ways
at the same time maintaining the vehicle's performance as usual. The goal of this work is to …

Mitigation of boundary layer separation and aerodynamic drag form the key objectives that
allow the aerial platforms to access greater efficiency and a wider operation envelope. Both …

Shock Wave Boundary Layer Interaction Control has been an active area of research for the
past decades. The effect of SWBLI on the flow filed and on the performance of Supersonic …

The purpose of this study is to assess the effect of turbulence modeling on the flow field and
on the performance of supersonic air intake at designed Mach number. Various turbulence …