Shock wave boundary layer interaction (original) (raw)

AI-generated Abstract

Shock wave boundary layer interaction (SWBLI) is a critical phenomenon in high-speed aerodynamics, particularly relevant for aerospace applications such as rockets and supersonic vehicles. This interaction can negatively influence performance by inducing issues such as drag rise, flow separation, and shock unsteadiness. Despite significant advancements in numerical methods, including RANS and LES, capturing the complex dynamics and low-frequency motion associated with SWBLI remains a challenge. Current exploration also emphasizes the need for further investigation into the underlying mechanisms driving these fluctuations, particularly in more diverse geometries.

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