Reynolds Number Effects on the Richtmyer-Meshkov InstabilityThis presentation compares the results of two very different experimental studies of Richtmyer-Meshkov instability: shock tube experiments in which an air/SF6 interface is accelerated by a weak shock wave; and incompressible experiments in which a box containing two different density miscible liquids is impulsively accelerated by bouncing it off of a fixed coil spring. Both experiments are initiated with sinusoidal initial perturbations. The interface perturbation initially remains sinusoidal as it grows in amplitude, but eventually the interfacial vorticity concentrates into points, forming a row of line vortices of alternating sign. The Reynolds number based on vortex circulation ranges from 1,000 to 45,000 in these experiments. It is found that viscous effects have a large, quantifiable effect on the evolution of the individual vortices. The effects of viscosity on the overall perturbation amplitude, however, are small and will be compared to theory.
Document ID
20120009030
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Niederhaus, Charles (NASA Glenn Research Center Cleveland, OH, United States)
Vitaliy, Krivets (Arizona Univ. Phoenix, AZ, United States)
Collins, Brett (Arizona Univ. Phoenix, AZ, United States)
Jacobs, Jeffrey (Arizona Univ. Phoenix, AZ, United States)