A common denominator between conical-symmetry and conical shock interaction is the
spanwise pressure gradient, which perform more non-uniformity and its interaction flow is …

An experimental study is conducted on the interaction of a swept shock wave with a
turbulent boundary layer. The shock wave is generated by a sharp unswept fin in a Mach 2 …

We derive a scaling law for the characteristic frequencies of wall pressure fluctuations in
swept shock wave/turbulent boundary layer interactions in the presence of cylindrical …

The mechanisms of unsteadiness in nominally two-dimensional (2-D) shock/turbulent-
boundary-layer interactions (STBLIs) cannot be directly extended to three-dimensional (3-D) …

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

The structure and the frequency spectra of wall pressure fluctuations beneath a planar
turbulent boundary layer interacting with a conical shock wave at Mach number dB), with an …

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

Strong crossflow and swept separation are key aspects of the flow dynamics of 3-D shock
wave/boundary layer interactions. This study explores the global surface pressure field …

Shock/turbulent-boundary-layer interactions (STBLIs) are ubiquitous in high-speed flight and
propulsion applications. Experimental and computational investigations of swept, three …

The mechanisms underlying transition of a Mach 6 flat plate boundary layer with adiabatic
wall conditions are explored with Direct Numerical Simulations (DNS) using a high-order …