When supersonic or transonic flows encounter solid surfaces, shock waves and the viscous boundary layer interact in complex ways that profoundly influence aerodynamic performance and stability. A ...

The boundary layer in high Reynolds number flows is a thin region adjacent to solid surfaces where viscous forces and shear dominate despite the overwhelming inertia of the external stream. At ...

The control of small structures and fast modes needs not only more accurate values in the commonly used dimensions (, u, T, P), but also, in fact more essentially, the controls from more dimensions.

The findings could help improve the efficiency and structural safety of internal aircraft components and nozzles in ...

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