On Monday 07 August 2006 17:50, Andy Ross wrote:
> Note to all YASim aircraft authors: the first fix discussed
> below is correct and has to be applied, but will (or at least
> may) have the effect of modifying the solution results of all
> YASim aircraft (tails are likely to be more effective: that
> means aircraft will be more stable on the whole, but less able
> to achieve high AoA's at full elevator).  I'd be appreciative
> if everyone could take their favorite aircraft out for a spin
> and report changes -- some may need re-tuning.
>
> Maik Justus wrote:
> > Andy Ross wrote:
> > > Maik Justus wrote:
> > > > Therefore for an wing without flap, spoiler and slat
> > > > [...] no surface element is generated.
> > >
> > > Ah, OK.  Yes, this was indeed a bug; I'm kinda shocked
> > > that we never noticed this before, it's been there since
> > > the code was written.
> >
> > Here it (the patch) is.
>
> Applied.
>
> > But before testing it with any YASim aircraft: I probably
> > found another bug in surface.cpp. For "general lift" and
> > "flap-lift" the effect of stall is calculated in stallFunc()
> > resp FlapLift().
>
> Yup, that looks correct to me.  Applied.  I'm not sure what
> the points was of the extra 1.0 in the return value; maybe a
> holdover from an earlier version where this function returned
> a scalar coefficient, and not a force?
>
> > If the fuselage is large in comparison to the wing, this
> > amount can be rather high.
>
> I don't think that's correct.  As I read the code, you would
> get 1N of force per fuselage surface (of which there are maybe
> a few dozen across a large aircraft).  The first bug is a
> whopper.  This one is pretty much noise unless you're modeling
> an R/C aircraft; I'm not surprised it stayed hidden for so
> long.
>
> Andy

It's at times like this when I sort of regret trying to populate 
the FG hanger...

:)

Reading the comments in the commits, I think it will help 
things...

LeeE


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