Hi Oliver

Welcome to FG world.

I use vstab for lower wing on K5Y1 (Aka Tombo).
You can see K5Y1.xml to find what should be done.
The latest K5Y1 is available at CVS and:
http://macflightgear.sourceforge.net/home/aircraft/k5y1

There're some points you need to know:
- dihedral must be clearly specified, otherwise it will be set to 90 degree.
- two vstab tags are needed (for left wing and right wing) since vstab will not 
be mirrored.
- some attributes must be negative for the right wing (since dihedral > 90)

I put incidence attribute to vstab, but I'm not that sure if it works properly.
Does anyone know about this?
If none knows, I'll take a look at Yasim code some time later (I have no time 
tonight...)

Hope it helps.

Tat

On Jun 26, 2009, at 9:04 PM, Olivier Faivre wrote:

> Interesting. Will try both possibilities.
> if mstab is not use by the solver, What about biplane ? Not so clear anymore 
> in my mind...
>
> However, if i cannot set incidence to the mstab, my idea is dead...
>
> Olivier
>
>
> 2009/6/26 leee <l...@spatial.plus.com>
> On Thursday 25 Jun 2009, Maik Justus wrote:
> > Hello Olivier,
> >
> > Olivier Faivre schrieb am 25.06.2009 20:52:
> > > Hello guys,
> > > ...
> > > Actually, the wing is done with only one piece, 7° dihedral, no
> > > twist. Can I use the "mstab" command to specify the outer wing
> > > and the regular "wing" command for the inner one ?
> >
> > yes
> >
> > > In the readme file, I read this for mstab : these surfaces are
> > > not involved with the solver computation these surfaces are not
> > > involved with the solver computation...
> > >
> > > I'm not sure to well understand.
> >
> > if you define a yasim FDM you have to define two configurations
> > with different airspeed, typ. cruise and approach. Yasim modifies
> > lift and drag factors and the incidence of the wing to meet these
> > configurations. Therefore the incidence of a wing will be
> > modified by the yasim solver (only once - when the model is
> > loaded) while the incidence of a mstab is unchanged.
>
> I just thought I'd point out that the YASim solver sets the
> incidence for the <hstab> element, not the <wing> element.
>
> Thus, you can specify the incidence for the <wing>, but not for the
> <hstab>.  There is also an INCIDENCE control-axis in YASim, which
> should allow the <wing> element incidence to be changed in flight
> and I think the F-8E, which is shown on the FG aircraft download
> web-page, may actually use this.  However, when I've tried using
> the INCIDENCE control-axis with <vstab> or <mstab> elements, to
> simulate all-moving/slab tailfins/rudders (as in the BAC-TSR2) or
> all-moving canards (as in the SU-37) it has had no aerodynamic
> affect at all.
>
> YASim does indeed generate drag factors for <wing>, <vstab> and
> <mstab> elements, but it is possible to modify the the AoA related
> drag forces by including suitable <idrag> elements .  This seems to
> work well when you're trying to simulate all-moving tailplanes, for
> example, if you specify a very low <idrag> factor for the <hstab>
> element.
>
> I also experimented with using <mstabs> to more accurately model the
> correct shape of wings when developing the Canberra-B(I)8 YASim
> config but found that the solver does indeed ignore the <mstab>
> elements when working out its stuff.  While I could get it to
> solve, the effect was that of just having the very short inner wing
> panels.  The <vstab> and <mstab> elements do have directional
> effects however, and the control-surface sub-elements, such as
> <flapn> and <spoiler> will also have an effect.
>
> For the main lifting surface then, using a full-span <wing> element
> will give more accurate results than a combination of <wing> and
> <mstab> elements because the <mstab> elements will be ignored.
> Although this may seem less than ideal, it's possible to fine-tune
> the single <wing> element to get very close to the real world
> characteristics, and certainly closer than you could get with a
> <wing> and <mstab> combination.
>
> LeeE
>
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