epeimen on iling blen flo. pa 1. similai in iling flothe effects of swirl on internal turbulent...

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665 Experiments on swirling turbulent flows. Part 1. Similarity in swirling flows By K. S. YAJNIK AND Itiational Aeronautical Laboratory, Bangaloro, India (Received 22 September 1972 and in revised form 17 May 1973) The effects of swirl on internal turbulent flows are studied by conducting experi- nments on turbulent pipe flow with variable initial swirl. This first part of the study is primarily concerned with similarity laws. The mean velocity profiles, both away from and close to the wall, are found to adroit similarity representations at sufficiently large Reynolds numbers, provided that flow reversal does not take place near the entrance. While the wall law is not sensibly dependent on swirl, the velocity defect law in its extended form is sensitive to swirl. Further, a logarithmic skin-friction law is obtained in which only the additive coefficient depends on swirl. This coefficient is found to vary linearly with the swirl angle in the range of the present experiments.

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Page 1: Epeimen on iling blen flo. Pa 1. Similai in iling floThe effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable

665

Experiments on swirling turbulent flows. Part 1.Similarity in swirling flows

By K. S. YAJNIK AND

Itiational Aeronautical Laboratory, Bangaloro, India

(Received 22 September 1972 and in revised form 17 May 1973)

The effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable initial swirl. This first part of the studyis primarily concerned with similarity laws. The mean velocity profiles, bothaway from and close to the wall, are found to adroit similarity representationsat sufficiently large Reynolds numbers, provided that flow reversal does not takeplace near the entrance. While the wall law is not sensibly dependent on swirl,the velocity defect law in its extended form is sensitive to swirl. Further, alogarithmic skin-friction law is obtained in which only the additive coefficientdepends on swirl. This coefficient is found to vary linearly with the swirl angle inthe range of the present experiments.

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M.V.SUBBAIAH
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J. Fluid Mechanics, 1973, 60 (4), pp.665-687
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Page 3: Epeimen on iling blen flo. Pa 1. Similai in iling floThe effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable
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Page 5: Epeimen on iling blen flo. Pa 1. Similai in iling floThe effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable
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Page 7: Epeimen on iling blen flo. Pa 1. Similai in iling floThe effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable
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Page 11: Epeimen on iling blen flo. Pa 1. Similai in iling floThe effects of swirl on internal turbulent flows are studied by conducting experi-nment•son turbulent pipe flow with variable
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