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 …

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

In this paper, the authors describe an experimental demonstration of Nitric-oxide ionization
induced Flow Tagging and Imaging (NiiFTI) in near-surface velocimetry applications. The …

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 …

Understanding the receptivity of hypersonic flows to free-stream disturbances is crucial for
predicting laminar to turbulent boundary layer transition. Input-output analysis as a …

Aspects of transition mechanisms on a 14° sharp-nosed ogive cylinder at Mach 6 are
elucidated by considering linear and nonlinear disturbance evolution of freestream …

We investigate hypersonic boundary layer instability and receptivity for using Input/Output
(I/O) analysis. Our approach directly incorporates of effects of multiple modes of instability as …

View Video Presentation: https://doi. org/10.2514/6.2023-3708. vid A computational
approach is used to evaluate the parametric effect of geometric and thermal conditions on …