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 paper presents a computational study of double focused laser differential interferometry
(D-FLDI) measurements related to the second (Mack) mode instability. High-fidelity direct …

As part of NATO STO AVT-346 “Predicting Hypersonic Boundary-Layer Transition on
Complex Geometries,” coordinated experimental and computational studies were conducted …

The goal of the Hypersonic Integrated Flight Research and Experimentation (HIFLIER) flight
experiment was to measure second-mode boundary-layer instabilities and subsequent …

The ROTEX-T is a cone-flare geometry that exhibits a separation bubble at the compression
corner at relevant freestream conditions. The geometry was used in a flight test by the …

A modified version of focused laser differential interferometry (FLDI) is demonstrated with
adjacent beam pairs distributed along the optical axis. This feature is accomplished using …

This study introduces an improvement of focused laser differential interferometry (FLDI)
featuring an additional laser of a different wavelength to create adjacent beam pairs arrayed …

A direct numerical simulation (DNS) of a transitional hypersonic boundary layer about an
axisymmetric model was conducted and probed by a simulated focused laser differential …

Several experimental campaigns have been conducted across a number of Mach-6 facilities
on the hypersonic flow around a CCF (CCF) geometry with a 5° half-angle cone and a 12° …