TY - GEN
T1 - Experimental investigations of mach 3 shock-wave turbulent boundary layer interactions
AU - Bookey, Patrick
AU - Wyckham, Christopher
AU - Smits, Alexander
PY - 2005
Y1 - 2005
N2 - Experiments were conducted to study two shock/turbulent boundary layer interactions in a Mach 2.9 flow. The interactions comprise a 24° compression corner and a 12° reflected shock interaction at Reθ = 2400. These low Reynolds number flows were chosen to coincide with DNS accessible Reynolds numbers in order to make direct comparisons. Measurements included mean flow surveys, surface pressure distributions, surface flow visualizations and Filtered Rayleigh Scattering (FRS).
AB - Experiments were conducted to study two shock/turbulent boundary layer interactions in a Mach 2.9 flow. The interactions comprise a 24° compression corner and a 12° reflected shock interaction at Reθ = 2400. These low Reynolds number flows were chosen to coincide with DNS accessible Reynolds numbers in order to make direct comparisons. Measurements included mean flow surveys, surface pressure distributions, surface flow visualizations and Filtered Rayleigh Scattering (FRS).
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M3 - Conference contribution
AN - SCOPUS:84884960569
SN - 9781624100598
T3 - 35th AIAA Fluid Dynamics Conference and Exhibit
BT - 35th AIAA Fluid Dynamics Conference and Exhibit
T2 - 35th AIAA Fluid Dynamics Conference and Exhibit
Y2 - 6 June 2005 through 9 June 2005
ER -