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NASA NTRS · 19900051561

Effects of streamwise vorticity injection on turbulent mixing layer development

Abstract

This 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.

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BibTeXRIS

Bell, James H., Mehta, Rabindra D.. 1990-06-01. Effects of streamwise vorticity injection on turbulent mixing layer development. https://ntrs.nasa.gov/citations/19900051561

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