Instability and transition onset downstream of a laminar separation bubble at Mach 6
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 …
sharp cone-cylinder-flare with a flare angle under hypersonic quiet flow. Two distinct …
Measurements of an axisymmetric hypersonic shear-layer instability on a cone-cylinder-flare in quiet flow
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 …
geometry with a 5∘ half-angle sharp cone were studied in the Boeing/AFOSR Mach-6 Quiet …
Quantitative focused laser differential interferometry with hypersonic turbulent boundary layers
The effect of turbulent wind-tunnel-wall<? TeX 2pc 0pt?> boundary layers on density change
measurements obtained with focused laser differential interferometry (FLDI) was studied …
measurements obtained with focused laser differential interferometry (FLDI) was studied …
Focused Laser Differential Interferometry: Recent Developments and Applications for Flow Measurements
Focused laser differential interferometry (FLDI), first introduced in the 1970s, has developed
into a powerful tool for the analysis of turbulent dynamics and fluctuations in fluid flows …
into a powerful tool for the analysis of turbulent dynamics and fluctuations in fluid flows …
Optical-axis spatial sensitivity of a simulated focused laser differential interferometer
A focused laser differential interferometer (FLDI) simulation was used to study the sensitivity
of the FLDI technique to a variety of factors. The model takes in a series of density fields and …
of the FLDI technique to a variety of factors. The model takes in a series of density fields and …
Effect of Angle of Attack on Separation Bubble Instability and Transition on a Cone-Slice-Ramp in Mach-6 Quiet Flow
AA Francis, JS Jewell - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
The Boeing/AFOSR Mach-6 Quiet Tunnel (BAM6QT) at Purdue University was used to
investigate the effect of angle of attack on three-dimensional compression-induced shock …
investigate the effect of angle of attack on three-dimensional compression-induced shock …
Separation and transition on a cone-cylinder-flare: Experimental campaigns
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 …
on the hypersonic flow around a cone-cylinder-flare (CCF) geometry with a 5 ^∘ half-angle …
Measurements on a blunt cone-cylinder-flare at mach 6
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 …
flare model was tested at the AFRL Mach-6 Ludwieg Tube at 0-degree angle of attack …
High-Speed Schlieren Visualization in Mach-6 Quiet Tunnel
B Price, Z McDaniel, SA Miller, S Overpeck… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1672. vid The Boeing/AFOSR
Mach-6 Quiet Tunnel (BAM6QT) at Purdue has lacked optical access for schlieren …
Mach-6 Quiet Tunnel (BAM6QT) at Purdue has lacked optical access for schlieren …
Hypersonic transitional boundary-layer profile using a linear-array FLDI
View Video Presentation: https://doi. org/10.2514/6.2023-4253. vid Simultaneous density-
fluctuation measurements were made using a linear array focused laser differential …
fluctuation measurements were made using a linear array focused laser differential …