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CYLEXPERT - Rotating Cylinder Electrode Intelligent Rotation Rate Calculator

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Corrosion Rate Calculator

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TUTORIAL ON CYLEXPERTTM AND THE ROTATING CYLINDER ELECTRODE

David C. Silverman


Table of Contents

Introduction-What is CYLEXPERT?
Overview of the Experimental Technique
Using CYLEXPERT-a step-by-step procedure
Hydrodynamics of a Smooth Cylinder
  1. Boundary Layer
  2. Mass Transfer Correlations
  3. Assessing Mass Transfer Control
         Models Relating Geometries
Effect of Surface Roughness
Wall Shear Stress vs. Mass Transfer
CYLEXPERT (The Intelligent Experimental Design Tool)
List of Symbols



Models Relating Geometries



That a measurement in one configuration can be used to predict if velocity sensitive corrosion exists in another configuration is an assumption. Part of its foundation comes from the observation that for the large Schmidt Numbers normally encountered in liquids the fully developed mass transfer boundary layer for hydraulically smooth surfaces is much thinner than the fully developed hydrodynamic boundary layer. The Schmidt number (raised to a fractional power) provides an order of magnitude ratio of the thicknesses of the hydrodynamic boundary to the mass transfer boundary layer. This relationship for liquids is depicted in this figure which assumes that the hydrodynamic boundary layer can be represented as having two sections, a thin viscous sublayer and a thicker turbulent outer layer. Since the flow is turbulent, the profiles are time-averaged profiles and are not drawn to actual scale.

Both boundary layer thicknesses are usually much smaller than the radius of curvature of the surface under study. Under these circumstances, the coordinate system within and immediately adjacent to the boundary layer may be assumed at least to a first approximation to be independent of the geometrical shape. For example, in the pipe and rotating cylinder electrode, these thicknesses are much less than the radii of curvature. That assumption is one of the main justifications for considering use of one geometrical configuration to predict the effect of fluid flow in another configuration. Such an approach is predicated on the additional provisos that the boundary layers in both geometries are fully developed and no detachment has occurred.

The objective, then, is to define experimental conditions in one geometry that can enable that geometry to model and predict the effect of fluid motion on corrosion in another geometry. Note that the word "predict" refers to corrosion mechanism, not corrosion rate. Two possible approaches have been proposed to establish flow conditions (rpm) within the rotating cylinder electrode that could enable predictions of velocity sensitive corrosion mechanisms in other geometries. These are similarity in wall shear stress (Silverman, D. C., Corrosion, 40(5), 220 (1984)1    (467k)) between geometries and similarity in mass transfer coefficients between that in the rotating cylinder electrode and that in the configuration of interest (Silverman, D. C., Corrosion, 44(1), 42 (1988)1    (522k)) and Nesic, S., Solvi, G. T., Skjerve, S, Br. Corros. J., 32(4), 269 (1997)). These references suggest that using the equivalence of mass transfer coefficients seems to provide a way to use one geometry to get a handle on corrosion in another if such corrosion is controlled by mass transfer and surface roughness is minimal. The linkage between geometries may be established, therefore, by determining fluid velocities in each that create equal mass transfer coefficients. The objective is to determine flow conditions under which to operate the rotating cylinder electrode so that the resulting corrosion mechanism and rate information will provide good insight about the mass transfer influence on corrosion mechanism in the modeled geometry. Good insight refers to understanding corrosion mechanism, not accurately determining corrosion rate.

After reviewing the equations that have been proposed (Silverman, D.C., Corrosion, 55(12), 1115 (1999)1    (271k)) those in the following table have been found to offer reasonable predictions for the geometries considered to relate fluid velocity in one geometrical configuration to that in the rotating cylinder electrode at equal mass transfer coefficients for hydraulically smooth surfaces. CYLEXPERT has extended this analysis to include several additional flow configurations important in industrial settings. Additional information can be found in D. C. Silverman, "The Rotating Cylinder Electrode for Examining Velocity-Sensitive Corrosion - A Review", Corrosion, Vol.60, No.11, p. 1003, 2004. 1    (1560k)

Geometry Relationship Source
Pipe Silverman
1988
Pipe Nesic
1997
Pipe Silverman
2003
Annulus Silverman
1988
Wall Jet Silverman
2003


This figure shows how the first 3 equations compare. The difference between the predictions of the first two equations is very slight. The third equation relating the rotating cylinder electrode to straight pipe flow was derived using a revised curve-fit and an alternative friction factor versus Reynolds number relationship for the rotating cylinder electrode, both of which might be better at higher Reynolds numbers. These equations could be used to relate velocities in the rotating cylinder electrode to those in the pipe as long as certain assumptions are fulfilled. Among them are (1) the hydrodynamic and mass transfer boundary layers are fully formed for the field geometry in question, (2) the surfaces are hydraulically smooth surfaces (roughness is absent or at most minimal), (3) interference from end effects is absent, (4) mass transfer plays an important role in creating fluid velocity sensitive corrosion, and (5) the boundary layers are attached. Note that including one experiment under static conditions is usually a good practice.

As discussed in the section entitled Effect of Surface Roughness surface roughness changes the Sherwood number vs. Reynolds number relationship because the mass transfer rate is usually increased by roughness. If increased roughness is suspected or observed, one might use the information provided by CYLEXPERT as a starting point. But instead of examining corrosion at only one or two rotation rates, the measurements should be made across a wider range of rotation rates and a plot generated in terms of Sherwood number versus Reynolds number. The line generated by curve-fitting the points may provide additional insight into the corrosion mechanism especially if the exponent deviates significantly from those values corresponding to a hydraulically smooth cylinder.






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1 © NACE International publication and year shown in citation above. All rights reserved. Displayed with permission from NACE International, Houston, TX (http://www.nace.org). Published in Corrosion, in the month and year shown in the citation above.






David C. Silverman, Ph.D. - Primary Consultant
E-Mail:     dcsilverman@argentumsolutions.com
Phone:     314-576-3586
Fax:         314-754-9825
Address:   The Argentum House
                14314 Strawbridge Ct.
                Chesterfield, MO 63017