Using Viscosity Instead of Drag
Substitute \(\boxed{\hat{\psi} = \underbrace{\psi_I}_{\text{Sverdrup streamfunction}}
+ \underbrace{\phi_W(\alpha,\hat{y})}_{\text{boundary layer correction}}}\) into \(\boxed{-\epsilon_M \nabla^4 \hat{\psi} + \frac{\partial \hat{\psi}}{\partial \hat{x}}
= \text{curl}_z \hat{\tau}_T}\) and subtract the Sverdrup balance. This gives
$$
-\epsilon_M\!\left(\nabla^4 \psi_I + \frac{1}{\epsilon^4}\frac{\partial^4 \phi_W}{\partial \alpha^4}\right)
+ \frac{1}{\epsilon} \frac{\partial \phi_W}{\partial \alpha} = 0
$$
A non-trivial balance occurs when
$
\epsilon = \epsilon_M^{1/3}
$
which implies a dimensional thickness $a\epsilon = (\nu/\beta)^{1/3}$
At leading order, equation \(\boxed{-\epsilon_M\!\left(\nabla^4 \psi_I + \frac{1}{\epsilon^4}\frac{\partial^4 \phi_W}{\partial \alpha^4}\right)
+ \frac{1}{\epsilon} \frac{\partial \phi_W}{\partial \alpha} = 0}\) reduces to
$$
-\frac{\partial^4 \phi_W}{\partial \alpha^4} + \frac{\partial \phi_W}{\partial \alpha} = 0
$$
The boundary conditions are that
- $\phi_W \to 0$ as $\alpha \to \infty$: this states that the perturbation decays as it extends into the interior
- $\phi_W = -\psi_I$ at $\hat{x} = \alpha = 0$: this is the no-normal-flow condition on the meridional boundary
- $\partial \phi_W / \partial \hat{x} = -\partial \psi_I / \partial \hat{x}$ at $\hat{x} = \alpha = 0$: this is the no-slip condition
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