Nikhil Mahalingesh [Opens in a new window], Experiments of transitional shock wave–boundary layer interactions (SBLIs) over 6 $^\circ$ and 10 $^\circ$ compression ramps were performed at Mach number 1 ...
Department of Mechanical and Aerospace Engineering, North Carolina State University, Raleigh, NC 27606, USA The dynamics of a shock-induced separation unit generated by a 20 $^\circ$ sharp fin placed ...
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