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"Climbing loop" / Acceleration
- Subject: "Climbing loop" / Acceleration
- Date: Tue, 28 Apr 2009 11:14:21 -0400
Walter & Group...
As some of you know, Phil Gay has spent years as
a military jet pilot and Navy aircraft carrier commander. Here is what he has to
say:
Gordy,
The jet pilot in me has to weigh in on the lift
issue again!
The fly line in itself can not generate lift.
Lift is caused when air comes across a fixed airfoil. The air
separates at the front of the airfoil and has to travel faster across the top
because of the camber in the airfoil. Even if you want to make the loop an
airfoil in order for lift to work both legs must be static. When shooting
neither leg is static and when not shooting only the bottom leg is
static. A rising loop is caused most like from trajectory not true
aerodynamic lift. Remember the Bernoulli principle is that as a fluid
(air) accelerates the pressure drops. That is why an
aircraft is sucked up into the air not really lifted from under the wing.
Let's put this fly line lift issue to bed.
Phil
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Phil,
This makes sense to me.
While we can't deny the "climbing loop", it
can't really be caused by LIFT defined in aeronautical
physics.
To my list of things which I think might
explain this phenomenon, I should have added TRAJECTORY or LAUNCH
ANGLE.
As my old chemistry professor once said as an
experiment he was demonstrating turned out with an unexpected result, "IT'S
THE NATURE OF THE BEAST ! "
Gordy
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
COMMENT: I recall a paper by
Caroline Gatti-Bono (I think a physics student of Noel Perkins at the U. of
Mich.) entitled: EFFECT OF LOOP SHAPE ON DRAG-INDUCED LIFT OF FLY LINE
..
This appeared as an attachment to a message in
Al Crise's CCI Study Group this morning. Unfortunately, the attachment
didn't contain the equations or diagrams.
I remember this paper well. My take was
that the authors were using the term "LIFT" to mean elevation due to other
factors, not LIFT in an aeronautical
sense.
I'd archived it, but lost it in a computer
crash a while back. I'll try to get it and if successful, will post it as
an attachment for those interested.
G.
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
ACCELERATION
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Returning to Mark Milkovitch's excellant
question, we now have comments by Bruce Richards. Bruce's answers are preceded
by ****. I've also highlighted them in RED
:
From Mark Milkovitch...
In Bruce Richards' comments on the Kyte & Moran "Elite Caster" study
(I'm
sure he means the one entitled, "Going For Distance"), he makes the point
that the best casters have "a constant rate of acceleration".
Does this mean that no matter how fast the rod tip is moving there is a
constant amount of force on it to move it even faster ?
****I suspect this is true, but would have to
confirm to be sure. B.
... And is it the case that a constant rate of acceleration is more
effective than an increasing rate of acceleration ?
*****No question about this one, yes! If the
acceleration is exponential
there is little rod bend initially, a lot later,
which results in tailing
loops eventually.
B.
Bruce