Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets
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Title
Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets
Authors
Keywords
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Journal
PHYSICS OF FLUIDS
Volume 25, Issue 5, Pages 055106
Publisher
AIP Publishing
Online
2013-06-01
DOI
10.1063/1.4807071
References
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