On Mon, 22 May 2006 16:34:03 +0200, Torsten wrote in message 
<[EMAIL PROTECTED]>:

> Hi,
> 
> i am currently implementing some basic structural icing. 
> It is implemented in nasal and works like this:
> 
> - check outside air temperature, dewpoint and effective visibility in
> a timer  loop at low frequency
> - if temperature is in the potential icing range and equal to dewpoint
> and  visibility below a certain value, assume you are in cloud and
> propagate a  generated icing severity (trace,light,moderate,severe) to
> the property tree.  Since there is no information about the liquid
> water content of our generic  clouds, I use an algo to generate the
> severity of icing. - Another part checks the icing severity and
> calculates the icing level on  configurable icing sensitive areas
> (wing, prop, fuselage etc). 

..we could pick this out of weather data.  And we could do something
similar to this for thermals.   And contrails.

> These icing  levels can than be used to scale some lift and drag
> coefficients and change  the mass of the aircraft in the FDM 

.._which_ fdm?  Or all of them???

> and let your bird do some unexpected things. They can also be used for
> 3d model animations to make the ice  visible.

..clear air icing too?   :o)

-- 
..med vennlig hilsen = with Kind Regards from Arnt... ;o)
...with a number of polar bear hunters in his ancestry...
  Scenarios always come in sets of three: 
  best case, worst case, and just in case.




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