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Probe measures gas and liquid mass flux in high mass flow ratio two-phase flowsDeceleration probe constructed of two concentric tubes with separator inlet operates successfully in flow fields where ratio of droplet flow rate to gas flow rate ranges from 1.0 to 20, and eliminates problems of local flow field disturbances and flooding. Probe is effective tool for characterization of liquid droplet/gas spray fields.
Document ID
19720000545
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Burick, R. J.
(N. Am. Rockwell Corp.)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Subject Category
Mechanics
Report/Patent Number
LEW-11270
Report Number: LEW-11270
Accession Number
72B10546
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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