Technical Papers
Nov 19, 2014

Numerical Analysis of Cavitation Phenomenon in a Vaned Ring-Type Needle Valve

Publication: Journal of Energy Engineering
Volume 141, Issue 4

Abstract

Cavitation is a destructive phenomenon in industrial needle-type control valves. In order to reduce the damaging effects of cavitation, a circular row of vanes is used at the end section of the needle valve. By changing the path of flow at the end section of the valve and generating a spiral movement in fluid, these vanes increase the near-wall pressure; thus, cavitation intensity is reduced and the bubbles move away from the walls. In this study, the effect of vane camber angle on cavitation intensity and formation location has been investigated. The results show that by increasing the vane camber angle from 10° to 70°, the spiral movement of flow increases and cavitation intensity diminishes mildly; however, as the camber angle increases beyond 70°, the spiral flow movement increases considerably and there is a significant reduction in cavitation intensity. It should be mentioned that at camber angles less than 70°, the flow coefficient remains almost constant; but at angles greater than 70°, the flow coefficient diminishes, resulting in an increase of energy supply cost.

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Published In

Go to Journal of Energy Engineering
Journal of Energy Engineering
Volume 141Issue 4December 2015

History

Received: May 5, 2014
Accepted: Oct 15, 2014
Published online: Nov 19, 2014
Discussion open until: Apr 19, 2015
Published in print: Dec 1, 2015

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Authors

Affiliations

Hassan Gholami [email protected]
Dept. of Mechanical Engineering, Iran Univ. of Science and Technology, 16887 Tehran, Iran (corresponding author). E-mail: [email protected]
Hamidreza Yaghoubi [email protected]
Dept. of Mechanical Engineering, Iran Univ. of Science and Technology, 16887 Tehran, Iran. E-mail: [email protected]
Mansour Alizadeh [email protected]
Assistant Professor, Dept. of Mechanical Engineering, Iran Univ. of Science and Technology, 16887 Tehran, Iran. E-mail: [email protected]

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