A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Soaring
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Yaw String in a Spin



 
 
Thread Tools Display Modes
  #1  
Old January 16th 05, 09:03 PM
John Galloway
external usenet poster
 
Posts: n/a
Default

It means exactly the same rudder direction you apply
in any other, non spinning, yawed condition (how could
it be otherwise as the string doesn't change its mode
of action in a spin?). The front end of a yaw string
is stuck to the canopy and if the loose end is pointing
left in a spin you apply apply right rudder.

I have never heard of anyone referring to the front
end of the yaw string being the way that it is pointing.
If they do that in the States the wording could
be changed. However, since pilots have ingrained into
thenm the wording 'full opposite rudder' for spin recovery,
I would strongly suggest retaining the word 'opposite'
and referring to the loose end of the yaw string as
the way it points.

There is nothing new to learn in what I suggest - I
just picked it up from Reichmann's book. The change
in emphasisis just that the attention is directed to
the yaw string in any case of doubt rather than to
watching the houses whirling about.

John Galloway


At 19:00 16 January 2005, Greg Arnold wrote:
'Apply full rudder opposite to the direction of the
yaw string' -- what
does that mean? What is the direction of the yaw string?
If the loose
end of the yaw string is on the right side of the canopy,
is the
direction of the yaw string to the right, or is it
to the left?

I think you mean that if the loose end of the yaw string
is on the right
side of canopy, you apply right rudder? Or the opposite
of the normal rule?




The yaw string *always* points to the inside of a
spin
(according the Reichmann and others) and modifying
the teaching to 'apply full rudder opposite to the
direction of the yaw string' would be a more certain
way of choosing the life rudder pedal rather than
the
death one at low altitude




  #2  
Old January 16th 05, 10:06 PM
Shawn
external usenet poster
 
Posts: n/a
Default

John Galloway wrote:
It means exactly the same rudder direction you apply
in any other, non spinning, yawed condition (how could
it be otherwise as the string doesn't change its mode
of action in a spin?). The front end of a yaw string
is stuck to the canopy and if the loose end is pointing
left in a spin you apply apply right rudder.

I have never heard of anyone referring to the front
end of the yaw string being the way that it is pointing.


Really? I picked it up somewhere in my instruction. Something to the
effect of "Think of the yaw string as an arrow with the head attached to
the canopy. It points to the the rudder pedal you need to push to
coordinate."
Seemed very natural and simple to me.

Shawn
  #3  
Old January 16th 05, 11:30 PM
Tony Verhulst
external usenet poster
 
Posts: n/a
Default


Really? I picked it up somewhere in my instruction. Something to the
effect of "Think of the yaw string as an arrow with the head attached to
the canopy. It points to the the rudder pedal you need to push to
coordinate." Seemed very natural and simple to me.


Yes. I use this most often with transitioning power pilots who are
taught to "step on the ball" of the inclinometer ("step on the head of
the arrow"). With ab initio glider pilots I start with telling them to
add rudder on the opposite side of where the tail of the string is
pointing. If that doesn't work, I switch to the above.

Tony V.
  #4  
Old January 17th 05, 02:57 AM
Greg Arnold
external usenet poster
 
Posts: n/a
Default

John Galloway wrote:
It means exactly the same rudder direction you apply
in any other, non spinning, yawed condition (how could
it be otherwise as the string doesn't change its mode
of action in a spin?). The front end of a yaw string
is stuck to the canopy and if the loose end is pointing
left in a spin you apply apply right rudder.



Are you sure? Imagine a flat spin. If the loose end is pointing to the
left, doesn't that mean yoiu are spinning to the right? So don't you
want left rudder?


 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) Rich Stowell Aerobatics 28 January 2nd 09 02:26 PM
Spin Training JJ Sinclair Soaring 6 February 16th 04 04:49 PM
String in the middle does not protect you from a spin Jim Soaring 10 January 30th 04 02:57 PM
Cessna 150 Price Outlook Charles Talleyrand Owning 80 October 16th 03 02:18 PM
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) Rich Stowell Piloting 25 September 11th 03 01:27 PM


All times are GMT +1. The time now is 11:56 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.