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 …

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 …

The unsteady nature of the flow field around an Oberkampf geometry—defined as a cone
with a parallel slice on which a ramp is mounted—is experimentally studied in quiet Mach 6 …

Experimental investigations into the base flow characteristics of a slender cone at Mach 6
were performed over a range of unit Reynolds numbers from approximately 7x10^ 6/m to …

The modal decomposition methods formulate the governing equations of a system as a
linear combination of the various modes to provide a powerful means for examining the …

Pressure transducer, infrared heat transfer, and schlieren imaging data for a flared cone and
cone-cylinder-flare in Mach 6 quiet flow are presented. Flared cone pressure transducer …