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Why

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Drag

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Analysis

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is

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Necessary

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Observation

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of

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the

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tube

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settlers

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yielded

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interest

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in

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floc

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buildup

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and

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floc

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flow

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in

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tubes.

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As

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the

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flocs

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began

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to

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build

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up,

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some

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started

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to

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roll

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up

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the

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tubes

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and

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flow

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out

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into

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the

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effluent

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instead of falling back into the floc blanket. It was determined that a drag force was possibly preventing the flocs from settling out. The question remained, however, as to why smaller tubes at higher flow rates experienced the rolling flocs but not the larger tubes.
It was determined that velocity gradients vary with the tube diameter, and that the drag force was related to the velocity gradient at the tube wall. As the diameter decreased at the same

Latex
\large\[V_\alpha\]
the velocity profile maintains the same amplitude, increasing the maximum velocity gradient experience by a floc on the tube wall. The following analysis was performed to find the threshold velocity gradient that results in a drag force which exceeds the force due to gravity which would cause the flocs to slide down the tube.

Wiki Markup
 of settling out and fall back into the floc blanket. It was determined that a drag force was possibly preventing the flocs from settling out. The question remained, however, as to why smaller tubes at higher flow rates experienced the rolling flocs but not the larger tubes


{float:right|border=2px solid black}
!Plate Settler Spacing Research Fall 2008^Uniformflow.png|width=200px|height=250px!
*h5. Figure 1: Development of Uniform Flow*fully developed flow
{float}

h3. 

Velocity

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Gradients

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The

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Reynolds

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number

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and

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entrance

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region

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length

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were

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calculated

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to

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determine

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whether

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the

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flow

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through

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the

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tubes

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was

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transient

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or

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laminar.

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With

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Reynolds

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numbers

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below

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100

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the

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length

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of

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the

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entrance

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region

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was

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determined

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by

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the

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following

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equation:

Latex

\large
$l_e  = 0.06{\mathop{\rm Re}\nolimits}  \cdot d$

It was then determined that the flow though the tubes became fully developed very quickly.

Figure 1 shows the evolution from uniform to fully developed. The parabola represents the fully developed velocity profile through the tubes. It is clear from this image that flocs experience higher velocity gradients in the entrance region.

The next calculation involved the Navier Stokes equation for laminar flow through a cylindrical tube, as seen below.

Latex

INSERT EQUATION

It was then determined that the flow though the tubes became laminar very quickly. 

Figure 1 shows the evolution flow from uniform to laminar. The parabola represents the velocity profile through the tubes. It is clear from this image that flocs experience high velocity gradients along the sides of the profile. 

The next calculation involved the Navier Stokes equation for laminar flow through a cylindrical tube, as seen below.

 {latex}
\large
$\frac{{\partial v}}{{\partial r}} = \frac{1}{\mu }\left( {\frac{{\partial p}}{{\partial z}}} \right)R + c_1 $width=250px
{latex}


Final equation:

{latex}$

Final equation:

Latex
\large
$\frac{{\partial v}}{{\partial r}} = \frac{{4 \cdot V}}{R}$

{latex}

This

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equation

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was

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evaluated

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at

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R,

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the

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radius

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of

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the

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tube,

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to

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find

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the

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maximum

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velocity

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gradient

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at

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the

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tube

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walls.

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Table

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1

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lists

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the

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velocity

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gradient

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values

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for

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each

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tube

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at

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the

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test

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critical

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velocities.

Wiki Markup
 

{float:right|border=2px solid black|width=700}
{excel:file=PSS flow rate experiment^DataAnalysis_aguaclara.xls |sheet=Velocity Gradient Table}
*Table 1. Results: The Velocity Gradients for the Tested Critical Velocities*
{float}

In

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order

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to

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determine

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a

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minimum

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plate

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spacing

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for

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the

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tanks

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in

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AguaClara

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plants,

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a

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Navier

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Stokes

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equation

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for

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laminar

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flow

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between

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two flat plates

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was

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used.

Latex

 


 {latex}
\large
$\frac{{\partial u}}{{\partial y}} = \frac{1}{\mu }\left( {\frac{{\partial p}}{{\partial x}}} \right)y + c_1 $width=250px
{latex}

Final equation:


{latex}$

Final equation:

Latex
\large
$\frac{{\partial u}}{{\partial y}} = \frac{{3V}}{{2h}}$

{latex}

The

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minimum

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spacing

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for

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plate

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settlers

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can

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be

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determined

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using

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the

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above

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equations.

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The

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velocity

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gradients

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found

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in

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each

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tube

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over

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the

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range

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of

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critical

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velocities

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can

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be

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found

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in

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Table

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1.

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By

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comparing

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the

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velocity

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gradients

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in

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table

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1

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and

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the

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results

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table

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from

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the

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flow

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rate

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experiment

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it

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can

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be

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determined

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that

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once

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the

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velocity

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gradient

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in

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the

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tube

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reaches

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a

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certain

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value,

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failure

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occurs.

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From

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the

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data

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it

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appears

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that

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failure

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occurs

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around

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2.4

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1/s,

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as

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velocity

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gradients

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beyond

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this

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value

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correspond

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with

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failure

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in

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the

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two

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smallest

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tube

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sizes

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tested.

Drag on a floc

Wiki Markup
 



h3. Drag on a floc
{float:right|border=2px solid black}
!Drag on floc.png|width=90px|height=90px!
*Figure 2: Force Balance on a floc*
{float}

Figure

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2

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shows

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the

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force

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balance

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on

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a

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floc.

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As

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stated

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before,

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it

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is

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believe

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that

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when

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the

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drag

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force

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on

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a

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floc

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exceeds

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force

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due

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to

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gravity,

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the

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floc

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beings

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to

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roll

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up

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the

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tube.

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