Swept shock wave/boundary layer interactions occur widely in the internal and external
flows of supersonic and hypersonic aircraft, which can seriously affect aircraft stability and …

The separation length employed to scale unsteady phenomena in strong (separated)
nominally two-dimensional (2-D) shock/turbulent-boundary-layer interactions cannot be …

Three-dimensional flowfield measurements within a separated swept shock wave/boundary-
layer interaction are acquired using a four-camera tomographic particle image velocimetry …

In order to apply the air fin successfully and ensure the maneuverability of hypersonic
vehicle, a key problem to be studied urgently is the heat flux brought by the fin mounting …

The effect of plasma actuators on a swept shock-wave/boundary-layer interaction induced
by a sharp fin was investigated by means of Reynolds-averaged Navier–Stokes …

The unsteady properties of three-dimensional (3-D) swept shock/turbulent-boundary-layer
interactions (STBLIs) depend on the topology of the 3-D separation, and intuition gained …

SWEPT shock-wave/boundary-layer interactions (SWBLIs) com-monly occur in supersonic
and hypersonic flows, which can easily cause flow separations [1, 2], severe …

High speed flows in engineering applications are often characterized by shock-
wave/boundary layer interactions (SWBLI) and three-dimensional flows. This thesis aims to …

Substantial research has been completed towards understanding and simulating
shock/boundary-layer interactions, but efforts have only recently begun to understand the …

Transient flow structures and surface heat flux distribution of the interfered flow field induced
by a backswept fin were obtained by Nano-tracer-based Planar Laser Scattering and …