From: "BD"
Newsgroups: warbirds.general
I also am a sailplane pilot, with some power time as well.
The effect you describe is known as adverse yaw. It is especially pronounced
in sailplanes because of the length of the wings, which give them a longer
moment arm (more leverage) Also, the ailerons are frequently proportionally
larger on a sailplane.
The effect does occur in power planes, but is often almost unnoticeable,
especially at higher speeds. When flying power, I have a tendency to overuse
the rudder. I find myself having to watch the rudder input carefully, since
too much rudder in a slow turn can cause the inside wing to stall, resulting
in a spin. Airline pilots will tell you that they almost never use the rudder
in a turn, even with the yaw damper turned off.
Adverse yaw is modelled in WB, but I have no idea how accurately, since
I am still waiting for my P-51 to be delivered.
From: "Finn"
Newsgroups: warbirds.general
I just got my solo student glider permit this summer. Starting powered
flight training this week.
It seems to take more rudder in general in gliders. My very small experience
agrees with yours. :)
Finn
From: Wells Sullivan
Newsgroups: warbirds.general
I think that because sailplanes have really long wings and the ailerons
are WAY out there...you get the effect more. It is modelled in WB. Fly a
Fw-190 and you should notice it. It may not be as noticeable on a computer
screen, cause you can't really feel anything and your perspective isn't
the same either (the screen is much smaller than your view in real life,
so any small changes in heading are less noticeable).
From: "Bjornar Svingen"
Newsgroups: warbirds.general
Another thing is that most planes (at least GA planes) have measures
to reduce adverse yaw. It can be unequal throw on the up and down movement,
for the same input the aileron that goes up goes let say 10 degrees while
the one that goes down only goes 2 degrees (just examples). Since only down
deflection will increase drag (higher effective aoa) you don't want all
that drag producing adverse yaw. Another commonly used measure is to make
the aileron and hinges so that a small part of the aileron that go up, also
goes down. The part that goes down only produces drag, so that the drag
will be more or less equal on both sides. And you can combine some of them.
I really don't know how it was done on the WWII birds, but I would guess
they had some of the same things as GA planes have today??
On gliders you will reduce drag as much as possible, so drag producing
devices is not used (I would think), and the long wings certainly doesn't
help.
From: Wells Sullivan <general6@iaw.com>
Newsgroups: warbirds.general
Most fighters do use the techniques that you mention. The Spitfire has
'frise' type ailerons, where the hinge line is back a bit, so that when
an aileron goes up, the leading edge of it goes down a little. The ailerons
also went up more than down. |