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 …
Instability measurements on a cone-slice-flap in Mach-6 quiet flow
AA Francis, K Dylewicz, A Klothakis… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
Reattachment behavior and shear-layer instabilities are investigated on a 7° cone, featuring
a slice parallel to its axis and a 20° compression ramp. Experiments and computations were …
a slice parallel to its axis and a 20° compression ramp. Experiments and computations were …
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 …
Application of Schlieren Methods to Flared Cone in Mach-6 Quiet Tunnel
ZA McDaniel, JS Jewell - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
Schlieren processing methods are applied to a flared cone geometry in a Mach 6 quiet
tunnel. High speed schlieren videos of laminar and transitional boundary layers over …
tunnel. High speed schlieren videos of laminar and transitional boundary layers over …
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 …
Instability and transition onset downstream of an axisymmetric separation bubble with sharp and blunt nosetips
View Video Presentation: https://doi. org/10.2514/6.2023-3702. vid A cone-cylinder-flare
model was tested at the Boeing/AFOSR Mach-6 Quiet Tunnel at 0-deg angle of attack …
model was tested at the Boeing/AFOSR Mach-6 Quiet Tunnel at 0-deg angle of attack …
Separation and Transition on the ROTEX-T Cone-Flare
J Davami, TJ Juliano, A Scholten, P Paredes… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
As part of NATO STO AVT-346 “Predicting Hypersonic Boundary-Layer Transition on
Complex Geometries,” coordinated experimental and computational studies were conducted …
Complex Geometries,” coordinated experimental and computational studies were conducted …
Nosetip bluntness effects on a cone-cylinder-flare at mach 6
A cone-cylinder-flare model with sharp and blunt nosetips was tested at the AFRL Mach-6
Ludwieg Tube at a 0\(^{\circ}\) angle of attack. Surface-pressure fluctuation measurements …
Ludwieg Tube at a 0\(^{\circ}\) angle of attack. Surface-pressure fluctuation measurements …
Transition to turbulence in hypersonic flow over a compression ramp due to upstream forcing
Several transition scenarios are present in a hypersonic compression-ramp flow. In our
previous work (Cao et al., J. Fluid Mech., vol. 941, 2022, p. A8), a complete transition …
previous work (Cao et al., J. Fluid Mech., vol. 941, 2022, p. A8), a complete transition …
Separation and transition on a cone-cylinder-flare: computational investigations
C Caillaud, S Esquieu, A Scholten, P Paredes… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
Base flow computation and stability analysis were conducted for hypersonic flow over a
cone-cylinder-flare (CCF) geometry for conditions that correspond to the experimental runs …
cone-cylinder-flare (CCF) geometry for conditions that correspond to the experimental runs …