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 …

This work focuses on detailed descriptions of DC discharge properties in supersonic airflow
and its applicability in combustion simulations. Due to the complexity of obtaining most of the …

Boundary layer transition has always been a frontier in the field of fluid mechanics, and
hypersonic boundary layer stability experiments can help reveal the physical mechanisms …

To improve the resistance capability of a dual-mode scramjet isolator, fluidic shock control
devices with different control parameters were designed. First, the effects of the control …

Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock
wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In …

The double-wedge configuration is a typical characteristic shape of the rudder surface of
high-speed aircraft. The impact of the shock wave/boundary layer interaction and the shock …

In the inlet passage of a hypersonic vehicle, multi-channel shock waves inevitably interact
with the boundary layer, producing complex multi-channel shock wave/boundary layer …