KR> Gs and aerodynamic lift

2008-10-12 Thread Colin & Bev Rainey
Orma and netters
First off lift is NOT created by a tugging of the wing panel up into the air. 
It is created by a combination of the deflected air PUSHING the bottom wing 
panel up (Newton's Law) and the airflow being increased over the top creating a 
pressure differential from under to over causing the air on the bottom to push 
up into the now low pressure area above the wing (Bernoulli's Law). The only 
force "sucking" on the wing skin is the small semi-vacuum created by the low 
pressure area of the airflow over the upper wing.  Negative Gs are simulated by 
adding weight to the UPPER wing panel, simulating the reverse G force hence 
negative of the wing attempting to produce lift downward in relationship to the 
pilot. Positive Gs are tested with the wing inverted, simulating the increased 
lifting force beyond 1G that is created when one increases the load on the wing 
during say a steep turn, pull-up, snap roll, etc... 1G is created when the 
aircraft is in equilibrium in straight and level flight, and this is increased 
when you decide to make a turn, which you can feel is the force pulling down on 
you during the maneuver. You have increased the amount of lift required over 
straight and level because now you are "borrowing" some other lift for straight 
and level to apply in the direction of the turn, so to remain level, lift must 
increase. There is a good chart in the Airplane Flying Handbook which 
illustrates very clearly the increasing Gs for the angle of bank of a given 
"level" non descending coordinated turn. Orma you are right, that the outside 
wing increases lift, with the down application of aileron, while the inboard 
wing decreases lift, each having an associated change in drag which causes 
adverse yaw. Application of the rudder is used to correct the adverse yaw. In 
the KR the differential ailerons, those that deflect up different from down, 
"tunes" out most of this adverse yaw for us making it simpler to fly 
coordinated.

The confusion may have come from looking at drawing that illustrate the lift 
"vectors" which are showing the resulting forces, and their direction of 
action, and misinterpret this to mean that that is where the force originates 
from.

2 Books for further reading that will enhance a pilot's understanding, and 
should be read completely, are the Pilot's Handbook of Aeronautical Knowledge, 
and the Airplane Flying Handbook. Both available at any decent pilot store, 
King School and Sportys Catalog and online ordering. They run about $14.95 each 
and will answer most of these questions in greater detail. If anyone has any 
other pilot questions like this, or related to flying, e-mail off the net and I 
will be glad to discuss them with you.

FLY SAFE!!!

Colin & Bev Rainey
KR2(td) N96TA
Sanford, FL
crain...@cfl.rr.com
http://kr-builder.org/Colin/index.html


KR> Gs and aerodynamic lift

2008-10-12 Thread larry severson

>First off lift is NOT created by a tugging of the wing panel up into the 
>air. It is created by a combination of the deflected air PUSHING the 
>bottom wing panel up (Newton's Law)

Very slight, unless at high speed (much higher than a KR2).

>  and the airflow being increased over the top creating a pressure 
> differential from under to over causing the air on the bottom to push up 
> into the now low pressure area above the wing (Bernoulli's Law).

Significant, and the reason that wing profiles change based on the speed 
range that the plane is designed to operate under.

>The only force "sucking" on the wing skin is the small semi-vacuum created 
>by the low pressure area of the airflow over the upper wing.

True, but not slight.

>Negative Gs are simulated by adding weight to the UPPER wing panel, 
>simulating the reverse G force hence negative of the wing attempting to 
>produce lift downward in relationship to the pilot.

I do not understand. Negative Gs are the result of changing the direction 
of the plane's nose in a downward direction at a pace that exceeds 32 
ft/sec squared. That is why one can encounter negative Gs with an abrupt 
leveling off at the end of a climb.

>Positive Gs are tested with the wing inverted, simulating the increased 
>lifting force beyond 1G that is created when one increases the load on the 
>wing during say a steep turn, pull-up, snap roll, etc...

Positive Gs are the result of pulling the nose up from the existing line of 
flight. A 60 degree level turn requires a 2G force applied to the plane by 
the pilot back pressure on the stick. An inside loop results in constant 
positive Gs, but an outside loop is all negative Gs.

>1G is created when the aircraft is in equilibrium in straight and level 
>flight,

True.


>FLY SAFE!!!

Larry Severson
Fountain Valley, CA 92708
(714) 968-9852
lar...@socal.rr.com