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NASA NTRS · 19840042947

Turbulence measurements in shock induced flows

Abstract

Turbulence measurements have been made in the incident and reflected flows of a shock tube. For the incident flow, M = 0.47 and Re/in. between 25,000 and 170,000 whereas in the reflected region M = 0.15 and Re/in. is between 12,000 and 85,000. Hot wire anemometers have been used to measure mass flux and total temperature fluctuations. In the incident flow mass flux and total temperatures averaged 1.2 percent and 0.5 percent respectively. The reflected shock amplified the turbulence intensities by approximately a factor of three. In general the intensities decreased with increasing flow Reynolds numbers.

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BibTeXRIS

Trolier, J. W., Duffy, R. E.. 1984-03-01. Turbulence measurements in shock induced flows. https://ntrs.nasa.gov/citations/19840042947

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