The shock wave/boundary-layer interaction is a common phenomenon, and it occurs in the
internal and external flow fields of the hypersonic vehicle. Then, the separation, the …

Molecular tagging measurement technique is an advanced non-intrusive visualization
approach which uses the molecules as the tagging and tracking materials. This technique …

We employ global input–output analysis to quantify amplification of exogenous disturbances
in compressible boundary layer flows. Using the spatial structure of the dominant response …

In the present work, a non-intrusive diagnostic technique known as molecular tagging
velocimetry was used to collect quantitative freestream velocity measurements in the Mach 7 …

The interfacing of measurement instrumentation to small computers for the purpose of online
data acquisition has now become standard practice in the modern laboratory. Computerized …

A parametric study of ramp-induced planar shock-wave/turbulent-boundary-layer
interactions (SBLIs) is carried out at hypersonic conditions (Mach number 6.0) by means of …

Shock-wave/boundary-layer interactions (SWBLIs) are critical phenomena in the design of
high-speed vehicles as they exhibit inherent unsteadiness that can damage airframes and …

The evolution characteristics of the mean skin friction beneath the supersonic turbulent
boundary layer that interacts with incident shock waves at Mach 2.25 are analyzed using …

Acetone tagging velocimetry (ATV) with nominally 1% mole fraction acetone seeding was
conducted in a shock-tunnel-generated hypersonic turbulent boundary layer over a hollow …

In this paper, we investigate the boundary-layer profiles that form over a sharp, hollow
cylinder in supersonic air and N 2 flows with a krypton tagging velocimetry (KTV) single …