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<DIV><FONT face=Arial size=2>I completely agree with the point Don is making
here. A snap is always just one of many elements in a maneuver. I feel that too
many people are fearing the "snap-nazis" who are going to come in and give them
a zero just because they didn't see a defined break. Most of the snaps I've
judged this year were not downgraded because I didn't see the break, I
downgraded them for differing radii, differing line lengths, off-center, and
stopping the auto-rotation prior to completion of the number of turns for the
snap. There's a difference between not doing a snap, and not showing a break
long enough for the judge to see it. The way I see it, if you didn't see the
break, but you saw the conical shape drawn by the rotation the only deduction
should be a 1-point per 15 degree rule applied to the angle the wings were at
when the body of the plane first deviates from level. Good luck seeing that (see
what Dave Lockhart just posted). If you didn't see it, or even if you think you
saw it and aren't sure, you can't downgrade for it. We need to get back to
watching the WHOLE maneuver, not just focusing on trying to catch someone
leaving out the most nit-picky part of one little part of the
maneuver.</FONT></DIV>
<DIV><FONT face=Arial size=2></FONT> </DIV>
<DIV><FONT face=Arial size=2>Matt</FONT></DIV>
<BLOCKQUOTE
style="PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; BORDER-LEFT: #000000 2px solid; MARGIN-RIGHT: 0px">
<DIV style="FONT: 10pt arial">----- Original Message ----- </DIV>
<DIV
style="BACKGROUND: #e4e4e4; FONT: 10pt arial; font-color: black"><B>From:</B>
<A title=don.ramsey@suddenlink.net href="mailto:don.ramsey@suddenlink.net">Don
Ramsey</A> </DIV>
<DIV style="FONT: 10pt arial"><B>To:</B> <A
title=nsrca-discussion@lists.nsrca.org
href="mailto:nsrca-discussion@lists.nsrca.org">'General pattern
discussion'</A> </DIV>
<DIV style="FONT: 10pt arial"><B>Sent:</B> Monday, June 16, 2008 5:36 PM</DIV>
<DIV style="FONT: 10pt arial"><B>Subject:</B> Re: [NSRCA-discussion] Snap
entry in FAI</DIV>
<DIV><BR></DIV>
<DIV class=Section1>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'">This
was the briefing at the world championship a couple of years ago.<SPAN
style="mso-spacerun: yes"> </SPAN>If it’s not a barrel roll and not an
axial roll, it’s probably a snap.<SPAN style="mso-spacerun: yes">
</SPAN>My guess is there were few if any 0’s on snaps in the semi-finals and
finals in this contest.<o:p></o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'"><o:p> </o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'">Here’s
my problem.<SPAN style="mso-spacerun: yes"> </SPAN>Let’s say the
maneuver is 45 downline snap.<SPAN style="mso-spacerun: yes"> </SPAN>The
pilot flies a small radius into the maneuver, a short line then the snap.<SPAN
style="mso-spacerun: yes"> </SPAN>Let’s say the snap is textbook.<SPAN
style="mso-spacerun: yes"> </SPAN>The judges look down and write the
score.<SPAN style="mso-spacerun: yes"> </SPAN>I can only assume it’s a
10.<SPAN style="mso-spacerun: yes"> </SPAN>Now continuing on, the line
after the snap is long and the last radius is very smooth and large.<SPAN
style="mso-spacerun: yes"> </SPAN>The judges didn’t see those elements
so again I can only assume they awarded a 10 for the maneuver that is in
reality a 6 to 8.<SPAN style="mso-spacerun: yes">
</SPAN><o:p></o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'"><o:p> </o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'">It’s
too bad the major contest often revolve around how the snaps are scored and
many times disregarding the other elements of the maneuver.<SPAN
style="mso-spacerun: yes"> </SPAN>Maybe the world championship briefing
should be the criteria everyone uses and should be the textbook
definition.<SPAN style="mso-spacerun: yes"> </SPAN>Let your FAI rep
know.<o:p></o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'"><o:p> </o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'">Don<o:p></o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'"><o:p> </o:p></SPAN></P>
<P class=MsoNormal><SPAN
style="FONT-SIZE: 11pt; COLOR: #1f497d; mso-bidi-font-family: 'Times New Roman'"><o:p> </o:p></SPAN></P>
<DIV>
<DIV
style="BORDER-RIGHT: medium none; PADDING-RIGHT: 0in; BORDER-TOP: #b5c4df 1pt solid; PADDING-LEFT: 0in; PADDING-BOTTOM: 0in; BORDER-LEFT: medium none; PADDING-TOP: 3pt; BORDER-BOTTOM: medium none">
<P class=MsoNormal><B><SPAN
style="FONT-SIZE: 10pt; FONT-FAMILY: 'Tahoma','sans-serif'; mso-fareast-font-family: 'Times New Roman'">From:</SPAN></B><SPAN
style="FONT-SIZE: 10pt; FONT-FAMILY: 'Tahoma','sans-serif'; mso-fareast-font-family: 'Times New Roman'">
nsrca-discussion-bounces@lists.nsrca.org
[mailto:nsrca-discussion-bounces@lists.nsrca.org] <B>On Behalf Of </B>chris
moon<BR><B>Sent:</B> Monday, June 16, 2008 5:13 PM<BR><B>To:</B>
nsrca-discussion@lists.nsrca.org<BR><B>Subject:</B> Re: [NSRCA-discussion]
Snap entry in FAI<o:p></o:p></SPAN></P></DIV></DIV>
<P class=MsoNormal><o:p> </o:p></P>
<P class=MsoNormal style="MARGIN-BOTTOM: 12pt"><SPAN
style="FONT-SIZE: 10pt; FONT-FAMILY: 'Tahoma','sans-serif'; mso-fareast-font-family: 'Times New Roman'">Continuing:<BR><BR>We
can all agree what a loop looks like and all agree what an axial roll
<BR>looks like right? The problems begin when we get into the "stalled"
<BR>maneuvers -stalls, snaps,spins. Different planes behave and "look"
<BR>differently in the stall therefore there cannot be one standard "look"
<BR>for these maneuvers. Intuitively we know that different designs have
<BR>different airfoils and each plane has different wing loadings depending
<BR>on their weight and will stall differently. Back to aerodynamics 101 we
<BR>know that a wing stalls when you exceed it's critical angle of attack
<BR>and this angle does not change as far as that wing is concerned.
<BR>Different wings will of course have differing critical angles of attack
<BR>before they stall. So, differing wings designs must look differently as
<BR>they will reach critical angle at different times. The only thing that
<BR>changes is the speed at which the wing will stall if you try to maintain
<BR>level flight while reducing it's airspeed. So, does a plane need to
<BR>depart from it's original flight path to stall? NO. It just needs to
<BR>pivot around the c/g to take the wing past it's critical angle of
<BR>attack. The c/g of the airplane can absolutely maintain it's track
<BR>through the air. The speed of the rotation in a snap or spin will
<BR>depend on the airfoil and amount of control throws used as well as c/g
<BR>but the key is that you do not have to leave your c/g track through the
<BR>air to stall the wing. Period. Same for stalls at the entry to spins -
<BR>you can fly level and reduce airspeed while increasing pitch until you
<BR>bring the wing to and past it's critical angle of attack. This may be
<BR>15-20 degrees of nose up attitude - not some false 40-45 degree pitch up
<BR>designed to "show" the stall. Both wings are stalled and should count
<BR>as stalled. Period. They may look differently, but both are stalled and
<BR>correct. We need to get away from what "looks" right in a stalled
maneuver.<BR><BR>Chris<BR><BR>fire away.......<BR><BR>chris moon
wrote:<BR>> George - you have made an excellent point in that the interval
may by<BR>> "minuscule" and not overly noticeable to everyone. It is
absolutely<BR>> wrong for some to claim that you must "show" them as judge
an<BR>> exaggerated pitch up just to satisfy a personal interpretation of
the<BR>> maneuver. Just as is is absolutely wrong for those judges to
demand<BR>> another overly exaggerated pitch up as a stall entry to a
spin<BR>> maneuver. It is never the job of the participant to exaggerate
a<BR>> portion of a maneuver just to prove it exists, therefore your usage
of<BR>> the term "minuscule" in terms of the time interval between pitch
and<BR>> rotation is something we need to keep in mind.<BR>><BR>>
Chris<BR>><BR>> george w. kennie wrote:<BR>>> My lip is becoming
too painful from biting it, so I think I'm going to<BR>>> stick my nose
in here somewhere.<BR>>> I think I'm with Jon on this one.<BR>>>
My logic, however flawed, tells me that if I am flying my plane<BR>>>
straight and level and I input rudder, no matter how much, there is
no<BR>>> way that this input will induce a stall to the airframe.
Therefore, it<BR>>> seems to me, that the necessary force required to
stall the main<BR>>> lifting surface must come from the elevator. It
would further seem to<BR>>> me that this input must, by it's very nature
produce a pitching<BR>>> attitude to the fuselage whether positive or
negative. So I would have<BR>>> to conclude that the attitude "break"
referenced by the rule can only<BR>>> refer to a "pitch" break and would
be impossible to confuse with an<BR>>> attitude change induced by the
rudder seeing that the required result<BR>>> is to stall the main
wing.<BR>>> And yes Jon, I agree that it would be necessary to lead with
the<BR>>> elevator in order to bring about this attitude change before
rotation<BR>>> is started, however miniscule the interval might
be.<BR>>> Of course I'm still open to hearing other interpretations and
their<BR>>> validations as these observations are strictly
opinions.<BR>>> G.<BR>>><BR>>> ----- Original Message
-----<BR>>> *From:* Jon Lowe<BR>>> *To:*
nsrca-discussion@lists.nsrca.org<BR>>><BR>>> *Sent:* Monday, June
16, 2008 2:10 PM<BR>>> *Subject:* Re: [NSRCA-discussion] Snap entry in
FAI<BR>>><BR>>> Jim,<BR>>><BR>>> I have no clue how
you think all three axes can be initiated at<BR>>> the same time. You
keep forgetting the part of the RULE, quoted<BR>>> verbatim below, that
says the "fuselage break and separation from<BR>>> the flight path" must
happen "BEFORE THE ROTATION IS STARTED". I'm<BR>>> NOT equating
fueselage break to pitch break, it could break in<BR>>> pitch and/or
yaw, if it doesn't start rotation at the same time.<BR>>> If you
initiate all three axis at the same time, rotation WILL<BR>>> start at
the same instant, and that is specifically NOT permitted.<BR>>> READ THE
RULE! The judge MUST determine if the fuselage broke and<BR>>> separated
from the flight path first, BEFORE the rotation started.<BR>>> If it
didn't, he MUST severely downgrade.<BR>>><BR>>><BR>>> Jon
Lowe<BR>>><BR>>><BR>>> -----Original
Message-----<BR>>> From: Woodward, Jim (US SSA)<BR>>> To: General
pattern discussion<BR>>> Sent: Mon, 16 Jun 2008 12:37 pm<BR>>>
Subject: Re: [NSRCA-discussion] Snap entry in FAI<BR>>><BR>>>
Jon,<BR>>><BR>>> I’m shocked - you are totally wrong here. Do not
equate “fuselage”<BR>>> to “pitch” in the reading of this definition. As
a judge you<BR>>> should NOT apply a “pitch-assessment” pass/fail
criteria to<BR>>> judging FAI snap rolls. It is completely rejected. The
plane and<BR>>> therefore “fuselage” must autorotate about the flight
axis, which<BR>>> means that the nose and tail of the plane will move in
a conical<BR>>> fashion. The pilot can initiate with all 3 axis at one
time.<BR>>><BR>>> It is the responsibility of the judge to
determine if autorotation<BR>>> occurred, and not determine how or in
what order the pilot did it.<BR>>><BR>>> Thanks,<BR>>>
Jim<BR>>>
------------------------------------------------------------------------<BR>>>
*From:* nsrca-discussion-bounces@lists.nsrca.org<BR>>><BR>>>
[mailto:nsrca-discussion-bounces@lists.nsrca.org<BR>>> ] *On Behalf
Of<BR>>> *Jon Lowe<BR>>> *Sent:* Monday, June 16, 2008 1:21
PM<BR>>> *To:* nsrca-discussion@lists.nsrca.org<BR>>><BR>>>
*Subject:* Re: [NSRCA-discussion] Snap entry in FAI<BR>>> You are
correct, as long as there is no roll induced at the same<BR>>> instant.
I overlooked that possibility. Not sure how rudder alone<BR>>> will
induce the "supposed to be in a stalled condition" though!!<BR>>> There
are many attitudes (e.g. 45 down on center) where a judge<BR>>> could
not likely see a rudder departure alone first, and thus<BR>>> conclude
that departure did not occur before the roll departure<BR>>> started.
And a judge might also not see a pitch departure first on<BR>>> a end
box upline snap, but he could see rudder first. It is VERY<BR>>> clear
that simultaneous roll with either or both of the other axes<BR>>>
departures is NOT allowed as others have tried to state here. I<BR>>>
did say that pitch and yaw departure could happen simutaneously,<BR>>>
in my original post, as long as roll doesn't occur at the same
time.<BR>>> Jon Lowe<BR>>><BR>>><BR>>> -----Original
Message-----<BR>>> From: JShulman><BR>>> To: General pattern
discussion<BR>>>><BR>>> Sent: Mon, 16 Jun 2008 11:22
am<BR>>> Subject: Re: [NSRCA-discussion] Snap entry in FAI<BR>>>
Jon,<BR>>> I don't see where it says pitch break? Rudder first will
show<BR>>> attitude break and separation from the flight path. So if one
uses<BR>>> rudder and elevator first this is also correct.<BR>>>
Regards,<BR>>> Jason<BR>>> www.jasonshulman.com<BR>>>
www.shulmanaviation.com<BR>>>
www.composite-arf.com<BR>>><BR>>> -----Original
Message-----<BR>>> *From:*
nsrca-discussion-bounces@lists.nsrca.org<BR>>><BR>>>
[mailto:nsrca-discussion-bounces@lists.nsrca.org<BR>>> ]*On
Behalf<BR>>> Of *Jon Lowe<BR>>> *Sent:* Monday, June 16, 2008
12:11 PM<BR>>> *To:*
nsrca-discussion@lists.nsrca.org<BR>>><BR>>> *Subject:* Re:
[NSRCA-discussion] Snap entry in FAI<BR>>> I suggest people re-read the
definition ofsnap-rolls from the<BR>>> FAI sporting code. I did a few
minutes ago. Here it is:<BR>>> "5B.7.5. *SNAP-ROLLS*<BR>>> A
snap-roll (or flick roll/rudder roll) is a rapid<BR>>> autorotative roll
where the model aircraft is in a stalled<BR>>> attitude, with a
continuous high angle of attack<BR>>> Snap-rolls have the same judging
criteria as axial rolls as<BR>>> far as start and stop of the rotation,
and<BR>>> constant flight path through the manoeuvre is
concerned.<BR>>> At the start of a snap-roll, the fuselage attitude must
show a<BR>>> definite break and separation from the<BR>>> flight
path, before the rotation is started, since the model<BR>>> aircraft is
supposed to be in a stalled<BR>>> condition throughout the manoeuvre, If
the stall/break does<BR>>> not occur and the model aircraft
barrelrolls<BR>>> around, the manoeuvre must be severely downgraded
(more than 5<BR>>> points). Similarly, axial<BR>>> rolls disguised
as snap-rolls must be severely downgraded<BR>>> (more than 5
points).<BR>>> Snap-rolls can be flown both positive and negative, and
the<BR>>> same criteria apply. The attitude<BR>>> (positive or
negative) is at the competitor’s discretion. If<BR>>> the model aircraft
returns to an unstalled<BR>>> condition during the snap-roll, the
manoeuvre is severely<BR>>> downgraded using the 1 point/15
degree<BR>>> rule."<BR>>><BR>>> Note that "the fuselage
attitude must show a definite break<BR>>> and separation from the flight
path, before the rotation is<BR>>> started..." That means that
simultaneous pitch and rotation is<BR>>> specifically NOT permitted. I
would interpret it as meaning<BR>>> that pitch and yaw could
theoretically happen simultaneously,<BR>>> as long as no roll is
involved. Sorry Matt, the rules as<BR>>> written do NOT allow actuation
in all three axes<BR>>> simultaneously. The rule also states that a
constant flight<BR>>> path has to be maintained.<BR>>><BR>>>
Let's face it, the only way to prevent severe downgrading from<BR>>>
EVERY judge, not just some judges, is to have a pitch break<BR>>> first.
Takes any question away.<BR>>> Jon
Lowe<BR>>><BR>>><BR>>> -----Original
Message-----<BR>>> From: rcmaster199@aol.com<BR>>> To:
nsrca-discussion@lists.nsrca.org<BR>>><BR>>> Sent: Mon, 16 Jun
2008 10:46 am<BR>>> Subject: Re: [NSRCA-discussion] Snap entry in
FAI<BR>>> A "Flick" and a "Snap" roll are the same roll in full
scale<BR>>> aerobatics parlance and reference
material.<BR>>><BR>>> Do these mean the same thing in model
aerobatics? In my view,<BR>>> they do<BR>>><BR>>> The latest
FAI regs allow actuation of the three main axes<BR>>>
simultaneously...that is, the regs don't specifically<BR>>>
differentiate "Pitch Break" from other deviations. I don't<BR>>> think
they specifically require that the model must rotate<BR>>> about it's
flight path either, I don't believe (.....plane<BR>>> must rotate in a
conical fashion about the fight axis....).<BR>>> The model would
probably present the best if that's done, so<BR>>> pilots may want to
consider that when executing the maneuver.<BR>>><BR>>> In my take,
a rapid Pitch is desired to preload the wing.<BR>>> Contrary to popular
belief, both panels dot not have to stall<BR>>> for a snap to occur.
Quite the opposite. Upon rudder<BR>>> deflection, the port panel will
practically stall (lift much<BR>>> much less than the other panel) but
the starboard panel must<BR>>> be lifting to create the autorotation. If
both panels stall,<BR>>> the model will fall out of the sky for a
distance and a snap<BR>>> would not occur at the correct moment in
time<BR>>><BR>>> MattK<BR>>><BR>>> -----Original
Message-----<BR>>> From: Woodward, Jim (US
SSA)<BR>>>><BR>>> To: General pattern
discussion<BR>>><BR>>>><BR>>> Sent: Mon, 16 Jun 2008 8:47
am<BR>>> Subject: Re: [NSRCA-discussion] Snap entry in
FAI<BR>>><BR>>> Guys,<BR>>><BR>>> I thought the FAI
changes explicitly allowed flick rolls? The<BR>>> rule<BR>>>
reads, "... fuselage attitude must show a definite break and<BR>>>
separation<BR>>> from the flight path."<BR>>><BR>>> It does
not say, "MUST SHOW PITCH BREAK." Please DO NOT<BR>>>
ERROUNIOUSLY<BR>>> APPLY A PASS/FAIL MAJOR DEDUCTION initial assessment
to the<BR>>> snap roll.<BR>>> Watch the whole maneuver then render
your score.<BR>>><BR>>> A break and separation from the flight
path simply means that<BR>>> the nose<BR>>> and tail of the plane
must rotate in a conical fashion about<BR>>> the fight<BR>>> axis.
Yaw, roll, and pitch can all break at the same moment if<BR>>> that
is<BR>>> how the pilot does it.<BR>>><BR>>> Hey :) some
really handsome smart guy wrote some stuff at this<BR>>>
link<BR>>> below about snap rolls to help clarify how they are done in
IMAC.<BR>>><BR>>>
http://www.mini-iac.com/DesktopDefault.aspx?tabid=77<BR>>><BR>>>
thanks,<BR>>> Jim<BR>>><BR>>><BR>>>
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