Betz's law indicates the maximum power that can be extracted from the wind, independent of the design of a wind turbine in open flow. According to Betz's law, no turbine can capture more than 16/27 (59.3%) of the kinetic energy in wind..
Sure it is, but only by doing things that may look like "cheating" and add an exorbitant cost.
Use two rotors, one in front of the other. There are many variations of this. They could both act as turbines, in which case you can get just a bit over Betz. Note that this is based on frontal area, not total swept area. Some may call this cheating. Another method: Have the rear turbine act like a normal turbine, and the front one only extracts power from the tip area. That air goes around the outside of the rear turbine, and hence extracting power from it is all gain. The best you can do is Betz limit based on active swept area, but based on frontal area, that gets you to about 0.79.
Use the front rotor as a propeller. This can increase the size of the captured stream tube, and hence power output. The problem here is there is circulating power: Some of the turbine's power is used to run the propeller. Excess losses in the system can pile up to the point you do not make a profit.
A well designed duct can easily beat Betz based on rotor area, and can even do so on duct exit area.
I worked on a configuration called "dynamic inducer" that added winglets to the tips of a wind turbine. It could also exceed Betz based on frontal area.
Altough all of this can let you beat Betz based on frontal area, they all add extra blade area and cost. If you instead used that extra area and money to make a larger single rotor, you would get more power. That is why none of these ideas are actually used.
Nazaruddin Sinaga : There are different methods to calculate this value, but finally you will end up with the same value only. For example, from axial induction factor
In my understanding it will reduce, because it is the ratio of rotor power and wind power. For adjusting fluctuation in the grid, the wind turbines are set to rated speed. Therefore, rotor power is constant for above rated speed while wind power is increasing with respect to velocity.
Please have a look precisely on the derivation of the Cp. There are 4 assumptions, at least, and the use of Bernoulli equation. In Bernoulli equation there are 4 assumptions, at least. And please look carefully that Betz did not say anything about the flow regimes, laminar or turbulent. If you remember, is there any difference between laminar and turbulent Bernoulli equations? I hope this will guide us to the more accurate calculation of Cp, I hope....
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CP= Aerodynamic Efficiency * Mechanical Efficiency * Electric Efficiency
As you may know every turbine has some losses such as (bearing, gear tooth, windage, and electrical resistance) losses. So, there is no Ideal turbine (CP=1) in real life situation. This means that all of the power (kinetic energy converted per unit of time) would be converted to electrical power. No wind coming out of the downwind side of the turbine and no mechanical or electrical losses in the system.