For laminar boundary layers over a flat plate, the Blasius solution gives:
- the overall thickness (or height) of the boundary layer
is the kinematic viscosity
is the distance downstream from the start of the boundary layer
is the Reynolds Number
is the density
is the freestream velocity
is the dynamic viscosit
![u_0](http://upload.wikimedia.org/wikipedia/en/math/1/1/0/110a451bff14cf0501f2ebb7c418a581.png)
![\nu](http://upload.wikimedia.org/wikipedia/en/math/7/3/6/7368318dd3647eb6bbf6afaf6d26c48d.png)
![R e_x = \rho u_0 x/\mu](http://upload.wikimedia.org/wikipedia/en/math/5/5/9/55987cd5504b1e31d5a9e0c8fec389f0.png)
with
![\rho](http://upload.wikimedia.org/wikipedia/en/math/f/7/f/f7f177957cf064a93e9811df8fe65ed1.png)
![\mu](http://upload.wikimedia.org/wikipedia/en/math/b/7/2/b72bb92668acc30b4474caff40274044.png)
![\nu](http://upload.wikimedia.org/wikipedia/en/math/7/3/6/7368318dd3647eb6bbf6afaf6d26c48d.png)
Re_x=
![u_0](http://upload.wikimedia.org/wikipedia/en/math/1/1/0/110a451bff14cf0501f2ebb7c418a581.png)
![\nu](http://upload.wikimedia.org/wikipedia/en/math/7/3/6/7368318dd3647eb6bbf6afaf6d26c48d.png)
![\delta](http://upload.wikimedia.org/wikipedia/en/math/f/1/0/f10f03c9836c36537d2539196058bfa2.png)
![\delta](http://upload.wikimedia.org/wikipedia/en/math/f/1/0/f10f03c9836c36537d2539196058bfa2.png)
In my mesh I will make 30 layers on the body with a total thickness of 30 mm. The thinnest layer will be 0.3 mm thick. With an expansionratio of 1.15 I will need 33 layers for 30 mm
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