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An experimental study of plane mixing layer developmentMean flow and turbulence was measured in the near field of two plane mixing layers in air with a maximum velocity of 21 m/sec. The experimental rig enabled mixing layers of velocity ratios 0 and 0.46 to be generated simultaneously. Gases with both tripped and untripped initial boundary layers were studied. It was found that the two stream layer developed to the self preserving state in a distance much shorter than did the single stream layer which followed accepted criteria for the development distance. The asymptotic levels of the turbulence quantities in the two stream layer and the development of the single stream layer showed agreement with existing data. It is suggested that the two stream mixing layer should provide a better test case for the development of turbulence models and calculation methods than the single stream mixing layer.
Document ID
19850021659
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mehta, R. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Westphal, R. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:86698
A-85159
NASA-TM-86698
Report Number: NAS 1.15:86698
Report Number: A-85159
Report Number: NASA-TM-86698
Accession Number
85N29971
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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