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 …
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 …
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 …
Separation and Transition on a CCF: Experimental Campaigns
EK Benitez, C Caillaud, ZA McDaniel… - AIAA SciTech Forum …, 2024 - ntrs.nasa.gov
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° …
on the hypersonic flow around a CCF (CCF) geometry with a 5° half-angle cone and a 12° …