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The Stress Profile
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As in all theories, let us start with a definition and a
theorem.
Definition: The stress profile is a
curve for the stresses in the deflected rod; but without
specifying the size of the stresses.
The Bike-Mender's Theorem: The
deflection and the stress distribution (the stress
profile) in the deflected rod determines the action of a
rod.
The BM-theorem is equivalent to the Garrison/Carmichael
theory, that the rod action is determined by the Garrison
stress curve.
The important difference between a Garrison stress curve
and the stress profile is, that the Garrison curve is
calculated using arms of moments without considering the
deflection, that makes the stresses fictive and the curve is only valid for the
rod for which is was calculated. I do not
reject the Garrison stress curve, but I caution the use
of it.
Knowing the Garrison stress curve, we can calculate the
stress profile, and vice versa.
The programs do not consider a swell a the bottom of the
rods. In cases where it is obvious, that the Garrison
taper at the bottom is starting to swell, the diameters
have been changed to obtain a straight taper down to a
point 20" from the butt. This is in agreement with
Garrison's remark, that the tapering at the bottom should
be almost straight. Ref.:Garrison, page 237. The straight
taper at the bottom is a consequence of the stress being
uniform.
A Garrison stress curve for a rod with light tip will
transform into a straight line in the diagram for the
stress profile.
A Garrison curve for a regular or heavy tip will
transform into a straight line for the main length of the
rod and then decrease as a smooth curve.
Irregularities in the stresses will make themselves
apparent in a similar way in both diagrams.
Look at the diagrams for 206 further down.
A frequently asked question is: How important is it, that
the Garrison stress curve is smooth -without humps?
The answer is: We don't know how much we can deviate
from the theoretical curve without changing the action of
the rod. But humps on the curve will change the curvature
of the deflected rod, it will not be noticeable to the eye
- but the deflection curve will be wavy.
On the other
hand, just removing the humps from a wavy Garrison stress
curve may not result in a better rod. It could be that
the points that look like humps were the points that
charaterized the action of that particular rod, and the
points that looked most smooth were the points that
should be changed.
Garrison Rod 193
| Point |
Rod 193 |
193
modified |
Difference |
| . |
. |
. |
. |
| 0" |
0.06250 |
0.06250 |
0.00000 |
| 5" |
0.07000 |
0.06997 |
0.00003 |
| 10" |
0.09000 |
0.09031 |
- 0.00031 |
| 15" |
0.10600 |
0.10599 |
0.00001 |
| 20" |
0.11950 |
0.11950 |
0.00000 |
| 25" |
0.13200 |
0.13222 |
- 0.00022 |
| 30" |
0.14400 |
0.14413 |
- 0.00013 |
| 35" |
0.15600 |
0.15580 |
0.00020 |
| 40" |
0.16800 |
0.16751 |
0.00049 |
| 45" |
0.18100 |
0.18065 |
0.00035 |
| 50" |
0.19300 |
0.19349 |
- 0.00049 |
| 55" |
0.20600 |
0.20649 |
- 0.00049 |
| 60" |
0.21900 |
0.21949 |
- 0.00049 |
| 65" |
0.23300 |
0.23249 |
0.00051 |
| 70" |
0.24500 |
0.24482 |
0.00018 |
The first row in the tables above show the
diameters of Garrison's rod 193.
The second row has been modified by an amount less than
+/-0.00049", so it has no effect as far as the rod
builder is concerned. In fact the rod builder will say
that the two rods are identical.
When we look at the stress curves below, an idea of how
Garrison designed his rods emerges.
Changing the modified rod diameters less than
0.00040" in four places, turns the stress curve into
a straight line.
When we consider, that the stress curve for the deflected
rod is calculated from classical theory of elasticity,
well known to Garrison, it will be difficult to reject
the hypothesis, that Garrison's basic idea was to
calculate his tapers to give a uniform stress
distribution in the rods.
The diagram below compares Garrison stress curves. The
rod 193 is calculated using Garrison's truncated
diameters the other is calculated by the program NewUni.

Garrison Rod 201
This was Garrison's favorite fly rod, built with what
he called a "progressive" taper.

Clearly, the main part of the rod must have been
calculated for a uniform stress.
That leads to the conclusion, that a
"progressive" taper is just another word for
uniform stress.
But how do we interpret the stress at point at 5"
and 10"?
If we use NewUni to calculate the rod with a tip factor =
0, we get a difference in diameters in two places.
The Garrison curves below show, that something special
has been done to the diameters near the tip, a feature
that is characteristic for many of Garrisons rods.

Garrison Rod 206
Each of Garrison's rod tapers presents a puzzle.
For the 206 the solution could be that the stress
reduction starts at 30" below the tip, with a tip
factor = 5.
There are other possibilities. We could try calculating a
best fit for the stress profile, but it would result in
higher stresses for points 5" and 10", Which
would be contrary to everything Garrison said.
I do not want to use the easy explanation, that some
diameters are miscalculated. On the other hand, it would
be strange if there are no calculation errors. We all
made calculation errors in the pre-computer age.
And come to think of it, it's still possible.
The diagram shows, where we will get a difference in
diameter.

The difference between Garrison's 206 and the rod
calculated by NewUni is not significant. Except for one
point, they are within the tolerances obtainable even by
a skilled rod builder.
| Point. |
206 original |
206 Uni |
Difference |
| . |
. |
. |
. |
| 0" |
0.06300 |
0.06300 |
0.000 |
| 5" |
0.07800 |
0.07862 |
-0.001 |
| 10" |
0.10000 |
0.10050 |
0.000 |
| 15" |
0.11700 |
0.11696 |
0.000 |
| 20" |
0.13100 |
0.13096 |
0.000 |
| 25" |
0.14400 |
0.14400 |
0.000 |
| 30" |
0.15600 |
0.15618 |
0.000 |
| 35" |
0.16800 |
0.16812 |
0.000 |
| 40" |
0.18100 |
0.17975 |
0.001 |
| 45" |
0.19400 |
0.19150 |
0.003 |
| 50" |
0.20600 |
0.20578 |
0.000 |
| 55" |
0.22000 |
0.21985 |
0.000 |
| 60" |
0.23300 |
0.23347 |
0.000 |
| 65" |
0.24700 |
0.24705 |
0.000 |
| 70" |
0.26000 |
0.26041 |
0.000 |
| 75" |
0.27500 |
0.27395 |
0.001 |
| 80" |
0.28700 |
0.28738 |
0.000 |
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