Navier's friction boundary condition in the Navier-Stokes equations for fluid flow takes the form
- \nu\frac{\partial u}{\partial n}=\beta u, (1)
where \nu > 0 is a small viscosity, u tangential velocity, n unit normal into the fluid and \beta \ge 0 a skin friction coefficient. For \beta =0 this is a zero-friction slip condition, while for \beta large it is a no-slip condition u=0.
For given \nu >0 there is a break even between balancing fluid and friction forces when \beta\approx\sqrt{\nu} with \beta >\sqrt{\nu} causing substantial reduction of u creating a (laminar) boundary layer of width \approx\sqrt{\nu} with \frac{\partial u}{\partial n}\approx \frac{1}{\sqrt{\nu}}, and \beta <\sqrt{\nu} causing little reduction of u approaching a slip condition without boundary layer.
The drag crisis at \nu \approx 10^{-6} with Reynolds number Re\approx 10^6 signifies a change from laminar no-slip boundary layer to an effective slip condition from a turbulent boundary layer as explained here. This corresponds to a friction coefficient \beta\approx 10^{-3} indicating a switch to slip in accordance with measured skin friction coefficients:
A connection with potential flow with slip and formally \nu =0 can be made by observing that potential flow satisfies on the boundary
- \frac{\partial u}{\partial n}=-u,
and so for any \nu >0
Euler CFD can be supplemented with positive skin friction and independence of e. g. drag for small skin friction can be observed.
Note that (1) with \beta =0 forms a weak boundary layer to satisfy \frac{\partial u}{\partial n}=0, while residual stabilisation in Euler CFD does not create any boundary layer.
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