Goosh, I'm almost sorry I started this thread. While it has been informative
Mark Jones is the only one that answered the question. Will it make a
difference in the flying characteristics of a KR2s. His answer was No from
actual flying of the non conforming configuration. While this debate has
The downward aileron deflection of the upward going wing will stall
first.
You change the camber of the wing and increase the angle of attack,
Virg
On 12/13/2014 8:51 AM, Tinyauto--- via KRnet wrote:
>
> The idea of differential control having a side advantage of reducing the
Exactly. This condition can bite you low and real slow, like during a
landing flare or thereabouts. Back in the day of "rudder airplanes" when
aileron differential was not common, people talked about "aileron
reversal" at low speeds. The wing you wanted to go up, with its aileron
down, would st
In a turn, if you bank further, the downward moving wing's angle of attack
is decreased. You actually have to worry about the outside wing and the
increased angle of attack as it is moving. The reduced downward deflection
of the aileron helps in that aspect.
Chris Pryce
On Dec 13, 2014 8:51 AM, "T
The idea of differential control having a side advantage of reducing the
chance of stall is nonsense to me. Lets say we are flying along checking
out something on the ground and are in a moderately steep bank of maybe 30 de
grees and allow the airplane to get somewhat slow. It would seem i
At 07:51 AM 12/13/2014, you wrote:
>However I am just not grasping
>the idea of it "reducing the tendency for the wing to stall" part. Am I
>wrong?
>Kevin Golden
+
I think they are saying the wing is "slightly less likely" to stall
compared t
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