Instability measurements of an axisymmetric, laminar separation bubble were made over a
sharp cone-cylinder-flare with a flare angle under hypersonic quiet flow. Two distinct …

Instabilities generated in Mach-6 quiet flow about an axisymmetric cone-cylinder-flare
geometry with a 5∘ half-angle sharp cone were studied in the Boeing/AFOSR Mach-6 Quiet …

Hypersonic flow over a two-dimensional compression corner is investigated using
computational fluid dynamics and global resolvent analysis in this study, which is a …

Several experimental campaigns have been conducted across a number of Mach-6 facilities
on the hypersonic flow around a cone-cylinder-flare (CCF) geometry with a 5 ^∘ half-angle …

This research focuses on measurements of a convective shear-layer instability seen
naturally in quiet hypersonic flow. Experiments were carried out in the Boeing/AFOSR Mach …

View Video Presentation: https://doi. org/10.2514/6.2023-1245. vid A blunt cone-cylinder-
flare model was tested at the AFRL Mach-6 Ludwieg Tube at 0-degree angle of attack …

Supersonic flow over a hollow cylinder/flare with a free-stream Mach number of 2.25 is
numerically investigated in this study. Axisymmetric computational fluid dynamics …

View Video Presentation: https://doi. org/10.2514/6.2022-3855. vid The development of both
convective stationary perturbation as well as global instabilities in the vicinity of a laminar …

The development of both convective stationary perturbation and global instabilities in the
vicinity of a laminar separation bubble above an axisymmetric compression corner in …

View Video Presentation: https://doi. org/10.2514/6.2023-1436. vid Background-oriented
schlieren and infrared thermography measurements were made simultaneously on a …