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one reference values area. how is it possible?

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Old   August 28, 2012, 07:23
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Mateusz
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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?
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Old   August 28, 2012, 09:31
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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?
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Old   August 28, 2012, 10:34
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Re=460 000 , ok so i will contact you by PM in the end of the week
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Old   August 28, 2012, 10:54
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i will contact you by PM in the end of the week
My pleasure

what is the chord length of your wing?
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Old   August 28, 2012, 11:03
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tail- chord 0.1m , wing- chord 0,15 m
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Old   August 28, 2012, 12:53
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Originally Posted by Mateusz View Post
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?
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