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Sensitivity of the structure of untripped mixing layers to small changes in initial conditionsAn experimental study was conducted concerning the influence of small changes in initial conditions on the near- and far-field evolution of the three-dimensional structure of a plan mixing layer. A two-stream mixing layer with a velocity ratio of 0.6 was generated with the initial boundary layers on the splitter plate laminar and was nominally two-dimensional. The initial conditions were changed slightly by interchanging the high- and low-speed sides of the wind tunnel, while maintaining the same velocities, and hence velocity ratio. This resulted in small changes in the initial boundary layer properties, and the perturbations present in the boundary layers were interchanged between the high- and low-speed sides for the two cases. The results indicate that, even with this relatively minor change in initial conditions, the near-field regions of the two cases differ significantly. The peak Reynolds stress levels in the near-field differ by up to 100 percent, and this is attributed to a difference in the location of the initial spanwise vortex roll-up. In addition, the positions and shapes of the individual streamwise vortical structures differ for the two cases, although the overall structures differ for the two cases, although the overall qualitative description of these structures is comparable. The subsequent reorganization and decay of the streamwise vortical structures is very similar for the two cases. As a result, in the far field, both mixing layers achieve similar structure, yielding comparable growth rates, Reynolds stress, distribution, and spectral content.
Document ID
19920024291
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Plesniak, M. W.
(Stanford Univ. CA, United States)
Bell, J. H.
(Stanford Univ. CA, United States)
Mehta, R. D.
(Stanford Univ. CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-190803
JIAA-TR-107
NAS 1.26:190803
Report Number: NASA-CR-190803
Report Number: JIAA-TR-107
Report Number: NAS 1.26:190803
Accession Number
92N33535
Funding Number(s)
CONTRACT_GRANT: NSF MSM-88-15670
CONTRACT_GRANT: NCC2-55
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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