I was considering that as I typed my response to you. Basically, any nozzle will be nonisentropic, which means it has losses as it speeds up (converging nozzle) or slows down (diverging nozzle) the flow.
Let's think about this from an idealized standpoint, and I will discuss why this idea won't work in actuality later.
Let's assume a uniform wind speed ([1]this is not true) entering into your nozzle. There is a fixed amount of energy coming into the nozzle. No matter what, the same amount of energy will come out the other end but at a faster speed ([2]this is not true either). That wind, while faster, still has the same amount of energy. The wind turbine, therefore, will still generate, the *same* amount of energy because the total energy in the airflow did not change.
What you could do, though, is have an entrance much bigger than the exit; *but* the exit is the size of the rotor of the wind turbine. Then you are taking more energy and pushing it through a smaller area at the exit. You're still pushing the same *amount* of energy - but its now higher because the area at the entrance is much larger than the turbine itself ([3,4]again, not true).
[1]Wind turbines operate near the ground where they are inside the boundary layer of the earth. The velocity profile is not constant, and the direction changes depending on which way the wind is blowing. So, the equation 0xDEADBEEF gave you is no longer valid, and the nozzle would have to turn with the wind turbine into the wind as the wind changes direction.
[2] All nozzles are nonisentropic, which means they have losses, so the energy coming out will be slightly less than the energy coming in due to losses in heat/friction/noise.
[3] Wind Turbines are HUGE. The size of this nozzle would be prohibitively large.
[4] Wind Turbines cannot operate when the wind speed is too slow, or too *fast*. So if the wind is strong, you don't want to over speed the blades on the wind turbine with your nozzle, they will fail and fly off.