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TUTORIAL ON CYLEXPERTTM AND THE ROTATING CYLINDER ELECTRODE
David C. Silverman
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Table of Contents
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 |
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Silverman 1988 |
| Pipe |
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Nesic 1997 |
| Pipe |
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Silverman 2003 |
| Annulus |
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Silverman 1988 |
| Wall Jet |
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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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Previous Page: Hydrodynamics of a Smooth Cylinder
Next Page: Effect of Surface Roughness
Return to Table of Contents
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.
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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
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