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 » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Coordinated turns and the little ball



 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #29  
Old October 9th 06, 08:39 PM posted to rec.aviation.piloting
Walt
external usenet poster
 
Posts: 98
Default Coordinated turns and the little ball


Dudley Henriques wrote:
"new_CFI" wrote in message
...


I guess he means precession. If you roll fast enogh, your aircraft
acts as a gyroscope. Now apply a force perpendicular to the roll axis,
and the result will be a precession motion which can be pretty

impressive.



ok, I knew it must have soemthing to do with a gyro....I couldnt reason it
out...but this makes sence. I hope your right...or else ill just have to
go back to being confused again.


That's a shame it makes sense, as its not correct, and understanding all
things related to flying are worth knowing as a flight instructor. There's
really no reason for any instructor to be "confused" when a little research
will enhance understanding.
If you are actually interested in inertia coupling, perhaps a little bit of
research might bring you up to speed on it. If not, please accept my sincere
apology for having mentioned it.
Dudley Henriques


Googling "inertia coupling" I found this, which cleared things up a bit
(at least for me):

A few of the experimental aircraft encountered a new type of behavior
known as inertia coupling, a behavior that was not fully appreciated
until the F-100 and F-102 also encountered it. Inertia coupling
resulted from the tendency of the new generation of high-speed aircraft
to concentrate most of the weight in a long thin fuselage, a departure
from the distribution of subsonic fighters. The X-3 configuration is an
excellent illustration. Even though its high-speed performance was
disappointing, the X-3's unanticipated susceptibility to loss of
control from inertia coupling contributed to understanding the problem.
With much less weight in the wing and tail, the dynamic motion in a
maneuver could cause the inertia of the fuselage to overpower the
aerodynamic stabilizing forces of the wing and tail. In the worst cases
the pilot lost control and the resulting abnormal air loads caused
airframe structural failure. The early F-100A models are remembered as
a classic example of susceptibility to inertia coupling, although the
initial F-102A models also encountered the problem.

--Walt
Bozeman, Montana

 




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


All times are GMT +1. The time now is 10:54 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.