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Effects of streamwise vorticity injection on turbulent mixing layer developmentThis paper investigates the effect of injected strong streamwise vorticity on the structure and development of a plane mixing layer originating from tripped boundary layers. The experiments were conducted in a mixing layer wind tunnel consisting of two separate legs which were driven individually by centrifugal blowers. It was found that, while the vorticity injection increased the growth rate in the near-field, the asymptotic growth rate was reduced by a factor of about two, together with the peak Reynolds stress levels. The result is attributed to the effect of the relatively strong and short wavelength streamwise vorticity in making the spanwise structures more three-dimensional and slowing down their pairing process, thus reducing entrainment, and hence growth.
Document ID
19900051561
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bell, James H.
(NASA Ames Research Center Moffett Field, CA, United States)
Mehta, Rabindra D.
(Stanford University CA, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-1459
Report Number: AIAA PAPER 90-1459
Accession Number
90A38616
Funding Number(s)
CONTRACT_GRANT: NCC2-55
Distribution Limits
Public
Copyright
Other

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