Effect of periodic aerodynamic pulsation on flow over a confined butterfly valve

Effect of periodic aerodynamic pulsation on flow over a confined butterfly valve  An experimental investigation of the flowfield characteristics of a butterfly valve under periodic flow has been made. The results concern a valve at large angles corresponding to high area contraction ratios (K>0.3). In steady flow, the results show that the flowfield within the valve is conditioned by the internal jet formed in the trailing edge fluid area. For very high area contraction ratios (K>0.65), the equivalent diameter of that fluid area is the preponderant length scale of the flow. In periodic flow, an increase in the length scale of flow instabilities is observed. The reorganization length of the flow is, thus, shorter, producing a marked reduction in valve head-loss. This phenomen is maximum when the excitation frequency is close to the nominal instabilities frequency (found in steady flow). http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Experiments in Fluids Springer Journals

Effect of periodic aerodynamic pulsation on flow over a confined butterfly valve

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Publisher
Springer-Verlag
Copyright
Copyright © 1998 by Springer-Verlag Berlin Heidelberg
Subject
Engineering; Engineering Fluid Dynamics; Fluid- and Aerodynamics; Engineering Thermodynamics, Heat and Mass Transfer
ISSN
0723-4864
eISSN
1432-1114
D.O.I.
10.1007/s003480050241
Publisher site
See Article on Publisher Site

Abstract

 An experimental investigation of the flowfield characteristics of a butterfly valve under periodic flow has been made. The results concern a valve at large angles corresponding to high area contraction ratios (K>0.3). In steady flow, the results show that the flowfield within the valve is conditioned by the internal jet formed in the trailing edge fluid area. For very high area contraction ratios (K>0.65), the equivalent diameter of that fluid area is the preponderant length scale of the flow. In periodic flow, an increase in the length scale of flow instabilities is observed. The reorganization length of the flow is, thus, shorter, producing a marked reduction in valve head-loss. This phenomen is maximum when the excitation frequency is close to the nominal instabilities frequency (found in steady flow).

Journal

Experiments in FluidsSpringer Journals

Published: Sep 17, 1998

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