and time is my problem i have a deficit of it, i have to hurry up with calculations and finish my thesis because i would like to defence it for 3 weeks, but after that i can try do this, it will be very usefull in my next simulations ;], results of what values of turb.length scale do you want to compare?

turbulence length scale=0.4*$,C,0.25C,0.5C(C is chord) and some others also, will tell you after consulting. OK first you concentrate on your thesis and after that if you will still be interested then we will work together and try to reach at a point.
BTW i also asked about the Reynolds No of your simulations?

Re=460 000 , ok so i will contact you by PM in the end of the week :)

My pleasure :)

what is the chord length of your wing?

tail- chord 0.1m , wing- chord 0,15 m

Do you have any idea or guess what over what percent of the chord the fallow will be laminar?