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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