Thanks to fzero, I got some mathematical help finding the velocity field of the air.
https://www.physicsforums.com/threads/conformal-transformation-fluid-flow-over-surface-waves.818636/The shape of the wave is described by a trochoid.
The last curve, but inverted about the x-axis, describes the wave.
[itex]u_0 = a \theta – b \sin \theta[/itex]
[itex]v_0 = – a + b \cos \theta[/itex],
parameric in [itex]\theta[/itex].
a and b are constants where a>b.
[itex]u[/itex] is the horizontal coordinate.
[itex]v[/itex] is the vertical coordinate.
The wave velocity is [itex]c= \sqrt{\frac{g\lambda}{2 \pi}}[/itex] where g is the acceleration due to gravity and [itex]\lambda[/itex] is the wavelength.
The streamlines of air, in a coordinate system where the wave is stationary are
[itex]u = a \theta – b \sin \theta e^{-y}[/itex]
[itex]v = ay – a + b \cos \theta e^{-y}[/itex]
where y is held constant. The so called velocity potentials are found by holding [itex]\theta[/itex] constant and varying y.
At [itex]y=0[/itex], the wave surface,
[itex]u = a \theta – b \sin \theta[/itex]
[itex]v = – a + b \cos \theta[/itex].
These are the first two equations.
Over constant intervals of [itex][\theta][/itex], say every 5 degrees, we have a system of points where the velocity potential intersects the wave surface. The velocity, c is inversely proportional to spacing between points.
[itex]c^2 =(\frac{du}{d \theta})^{-2} + (\frac{dv}{d \theta})^{-2}[/itex]
[itex]\frac{du}{d\theta} = a-b cos(\theta)[/itex]
[itex]\frac{dv}{d\theta} = -b sin(\theta)[/itex]
A wave peak occurs where v is maximal; [itex]\theta= 0[/itex].
A trough is found at [itex]\theta=\pi[/itex].
At the peak
[itex]\frac{du}{d\theta}=a-b[/itex]
[itex]\frac{dv}{d\theta}=0[/itex]
and [itex]c^2=(a-b)^{-2}[/itex].
At the trough
[itex]\frac{du}{d\theta}=a+b[/itex]
[itex]\frac{dv}{d\theta}=0[/itex]
and [itex]c^2=(a+b)^{-2}[/itex].
The free stream velocity, high above the waves is [itex]c=1/a[/itex].
We can now apply Bernoulli, [itex]V^2+2p=H[/itex] to find the gage pressure at points along the wave. H is a constant.
For the free steam, we establish the value of H. [itex]H=c^2=\frac{1}{a^2}[/itex].
At a peak, [itex](a-b)^{-2}+2p= a^{-2}[/itex]
The pressure, [itex]p=(1/2)[(a-b)^{-2}-a^{-2}][/itex].
At a trough, [itex](a+b)^{-2}+2p= a^{-2}[/itex]
The pressure, [itex]p=(1/2)[(a+b)^{-2}-a^{-2}][/itex].
These are difficult to evaluate without some numbers. For a=1 and b=1/2, peak pressure is less than gauge over the peaks and greater than gauge over the troughs, as expected.
The pressure acts symmetrically about the peaks and troughs. This seems to mean that the pressure profile is in phase with the waves so that no energy is transferred in this idealized analysis and no violation of the conservation of energy.