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 …

View Video Presentation: https://doi. org/10.2514/6.2023-2438. vid A self-aligned focusing
schlieren (SAFS) apparatus based on a recently published design is implemented for the …

Femtosecond laser electronic excitation tagging (FLEET) velocimetry is applied in a
hypersonic boundary layer behind an array of turbulence-inducing trips. One-dimensional …

View Video Presentation: https://doi. org/10.2514/6.2023-0869. vid The reconstruction of
globally-consistent hypersonic boundary layer disturbance modes from experimental …

View Video Presentation: https://doi. org/10.2514/6.2023-0268. vid The effects of roughness
on shock-wave/boundary-layer interactions have been studied in the UTSA Mach 7 …

View Video Presentation: https://doi. org/10.2514/6.2023-0098. vid A series of experiments
were performed in the Air Force Research Laboratory Mach-6 Ludwieg Tube using a …

View Video Presentation: https://doi. org/10.2514/6.2023-0220. vid Femtosecond laser
electronic excitation tagging (FLEET) was applied to velocimetry on a hypersonic double-fin …

View Video Presentation: https://doi. org/10.2514/6.2022-3477. vid Femtosecond laser
electronic excitation tagging was applied in a transitioning boundary layer behind an array …

Ogive cylinders are representative designs of hypersonic forebodies and harbor several flow
complexities. This work evaluates the effects of nose bluntness of ogive-cylinder forebodies …

This research work studies the effects of surface roughness on shock-wave/boundary-layer
interactions (SWBLIs). SWBLI are prevalent in supersonic and hypersonic flows and occur …