Affiliation
Univ Arizona, Dept Aerosp & Mech EngnIssue Date
2017Keywords
Shock tubesFlow visualization
Richtmyer Meshkov instabilities
Gas liquid interfaces
Fluid mixing
Metadata
Show full item recordPublisher
AMER INST PHYSICSCitation
AIP Conference Proceedings 1793, 150003 (2017); doi: 10.1063/1.4971732Rights
© 2017, AIP Publishing LLC.Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
Richtmyer-Meshkov instability is studied in shock tube experiments with an Atwood number of 0.7. The interface is formed in a vertical shock tube using opposed gas flows, and three-dimensional random initial interface perturbations are generated by the vertical oscillation of gas column producing Faraday waves. Planar Laser Mie scattering is used for flow visualization and for measurements of the mixing process. Experimental image sequences are recorded at 6 kHz frequency and processed to obtain the time dependent variation of the integral mixing layer width. Measurements of the mixing layer width are compared with Mikaelian's [1] model in order to extract the growth exponent. where a fairly wide range of values is found varying from theta approximate to 0.2 to 0.6.Note
12 Month Embargo; Published Online: January 2017ISSN
0094-243XVersion
Final published versionSponsors
Lawrence Livermore National Laboratory; National Nuclear Security Administration under the Stewardship Science Academic Alliances programAdditional Links
http://aip.scitation.org/doi/abs/10.1063/1.4971732ae974a485f413a2113503eed53cd6c53
10.1063/1.4971732
