# Betz's law

(Redirected from Betz' law) Schematic of fluid flow through a disk-shaped actuator. For a constant-density fluid, cross-sectional area varies inversely with speed.

In aerodynamics, Betz's law indicates the maximum power that can be extracted from the wind, independent of the design of a wind turbine in uniformly transverse open flow on an aerodynamically thin wind harvester. It was published in 1919 by the German physicist Albert Betz. The law is derived from the principles of conservation of mass and momentum of the air stream flowing through an idealized "actuator disk" that extracts energy from the wind stream. According to Betz's law, no aerodynamically thin windmill of any mechanism can capture more than 16/27 (59.3%) of the kinetic energy in wind. The factor 16/27 (0.593) is known as Betz's coefficient. Practical utility-scale wind turbines achieve at peak 75–80% of the Betz limit.

The Betz limit is based on an open-disk actuator. If a diffuser is used to collect additional wind flow and direct it through the turbine, more energy can be extracted, but the limit still applies to the cross-section of the entire structure.

## Concepts Simple cartoon of two air molecules shows why wind turbines cannot actually run at 100% efficiency.

Betz's law applies to all Newtonian fluids, including wind. If all of the energy coming from wind movement through a turbine were extracted as useful energy, the wind speed afterward would drop to zero. If the wind stopped moving at the exit of the turbine, then no more fresh wind could get in; it would be blocked. In order to keep the wind moving through the turbine, there has to be some wind movement, however small, on the other side with some wind speed greater than zero. Betz's law shows that as air flows through a certain area, and as wind speed slows from losing energy to extraction from a turbine, the airflow must distribute to a wider area. As a result, geometry limits any turbine efficiency to a maximum of 59.3%.

## Independent discoveries

British scientist Frederick W. Lanchester derived the same maximum in 1915. The leader of the Russian aerodynamic school, Nikolay Zhukowsky, also published the same result for an ideal wind turbine in 1920, the same year as Betz. It is thus an example of Stigler's law, which posits that no scientific discovery is named after its actual discoverer.

## Proof

The Betz Limit is the maximum possible energy that may be derived by means of an infinitely thin rotor from a fluid flowing at a certain speed.

In order to calculate the maximum theoretical efficiency of a thin rotor (of, for example, a windmill) one imagines it to be replaced by a disc that withdraws energy from the fluid passing through it. At a certain distance behind this disc the fluid that has passed through flows with a reduced velocity.

### Assumptions

1. The disk does not possess a hub and is ideal (so if it were conceptualized as a rotor it might have an infinite number of blades, which have no drag). Any non-idealities are assumed to only lower this idealized value making it an upper bound.
2. As an effectively 1-D model, the flow into and out of the disk is axial, and all velocities are transversely uniform. This is a control-volume analysis, and to construct a solution, the control volume must contain all flow going in and out, failure to account for that flow would violate the conservation equations.
3. The flow is non-compressible. Density remains constant, and there is no heat transfer.
4. Uniform pressure is applied to the disk (again a 1-D model, so no radial dependence on pressure)

### Application of conservation of mass (continuity equation)

Applying conservation of mass to this control volume, the mass flow rate (the mass of fluid flowing per unit time) is given by

${\dot {m}}=\rho A_{1}v_{1}=\rho Sv=\rho A_{2}v_{2},$ where v1 is the speed in the front of the rotor, v2 is the speed downstream of the rotor, v is the speed at the fluid power device, ρ is the fluid density, the area of the turbine is given by $S$ , and $A_{1}$ and $A_{2}$ are the areas of the fluid before and after reaching the turbine.

So the density times the area and speed should be equal in each of the three regions: before, while going through the turbine and afterward.

The force exerted on the wind by the rotor is the mass of air multiplied by its acceleration. In terms of the density, surface area and velocities, this can be written as

{\begin{aligned}F&=ma\\&=m{\frac {dv}{dt}}\\&={\dot {m}}\,\Delta v\\&=\rho Sv(v_{1}-v_{2}).\end{aligned}} ### Power and work

The work done by the force may be written incrementally as

$dE=F\,dx,$ and the power (rate of work done) of the wind is

$P={\frac {dE}{dt}}=F{\frac {dx}{dt}}=Fv.$ Now substituting the force F computed above into the power equation will yield the power extracted from the wind:

$P=\rho Sv^{2}(v_{1}-v_{2}).$ However, power can be computed another way, by using the kinetic energy. Applying the conservation of energy equation to the control volume yields

$P={\frac {\Delta E}{\Delta t}}={\tfrac {1}{2}}{\dot {m}}(v_{1}^{2}-v_{2}^{2}).$ Looking back at the continuity equation, a substitution for the mass flow rate yields

$P={\tfrac {1}{2}}\rho Sv(v_{1}^{2}-v_{2}^{2}).$ Both of these expressions for power are completely valid, one was derived by examining the incremental work done, and the other by the conservation of energy. Equating these two expressions yields

$P={\tfrac {1}{2}}\rho Sv(v_{1}^{2}-v_{2}^{2})=\rho Sv^{2}(v_{1}-v_{2}).$ For all v and S the density cannot be 0. Examining the two equated expressions yields an interesting result, namely

${\tfrac {1}{2}}(v_{1}^{2}-v_{2}^{2})={\tfrac {1}{2}}(v_{1}-v_{2})(v_{1}+v_{2})=v(v_{1}-v_{2}),$ or

$v={\tfrac {1}{2}}(v_{1}+v_{2}).$ Therefore, the constant wind velocity across the rotor may be taken as the average of the upstream and downstream velocities. This is arguably the most counter-intuitive stage of the derivation of Betz's law. This strong result is directly a consequence of the "axial flow" assumption which disallows any massflow radial to axial flow in the actuator disk region. Without mass escape and a constant diameter to the actuator region the air Speed cannot change in the interaction region and thus no energy can be extracted other than at the front and back of the interaction region, fixing the airspeed of the actuator disk to be the average. (Removing that restriction may allow higher performance than Betz law allows but other radial effects should also be considered. This constant velocity effect is distinct from the radial kinetic energy loss that is also ignored.)

## Betz's law and coefficient of performance

Returning to the previous expression for power based on kinetic energy:

{\begin{aligned}P&={\tfrac {1}{2}}{\dot {m}}(v_{1}^{2}-v_{2}^{2})\\&={\tfrac {1}{2}}\rho Sv(v_{1}^{2}-v_{2}^{2})\\&={\tfrac {1}{4}}\rho S(v_{1}+v_{2})(v_{1}^{2}-v_{2}^{2})\\&={\tfrac {1}{4}}\rho Sv_{1}^{3}\left(1-\left({\frac {v_{2}}{v_{1}}}\right)^{2}+\left({\frac {v_{2}}{v_{1}}}\right)-\left({\frac {v_{2}}{v_{1}}}\right)^{3}\right).\end{aligned}}  The horizontal axis reflects the ratio v2/v1, the vertical axis is the power coefficient[bare URL] Cp.

By differentiating $P$ with respect to ${\tfrac {v_{2}}{v_{1}}}$ for a given fluid speed v1 and a given area S, one finds the maximum or minimum value for $P$ . The result is that $P$ reaches maximum value when ${\tfrac {v_{2}}{v_{1}}}={\tfrac {1}{3}}$ .

Substituting this value results in

$P_{\text{max}}={\tfrac {16}{27}}\cdot {\tfrac {1}{2}}\rho Sv_{1}^{3}.$ The power obtainable from a cylinder of fluid with cross-sectional area S and velocity v1 is

$P=C_{\text{p}}\cdot {\tfrac {1}{2}}\rho Sv_{1}^{3}.$ The reference power for the Betz efficiency calculation is the power in a moving fluid in a cylinder with cross-sectional area S and velocity v1:

$P_{\text{wind}}={\tfrac {1}{2}}\rho Sv_{1}^{3}.$ The power coefficient Cp (= P/Pwind) is the dimensionless ratio of the extractable power P to the kinetic power Pwind available in the undistributed stream.[citation needed] It has a maximum value Cp max = 16/27 = 0.593 (or 59.3%; however, coefficients of performance are usually expressed as a decimal, not a percentage).

Modern large wind turbines achieve peak values for Cp in the range of 0.45 to 0.50,[full citation needed] about 75–85% of the theoretically possible maximum. In high wind speed, where the turbine is operating at its rated power, the turbine rotates (pitches) its blades to lower Cp to protect itself from damage. The power in the wind increases by a factor of 8 from 12.5 to 25 m/s, so Cp must fall accordingly, getting as low as 0.06 for winds of 25 m/s.

## Understanding the Betz results

The speed ratio ${\tfrac {v_{2}}{v_{1}}}={\tfrac {1}{3}}$ between outgoing and incoming wind implies that the outgoing air has only $({\tfrac {1}{3}})^{2}={\tfrac {1}{9}}$ the kinetic energy of the incoming air, and that ${\tfrac {8}{9}}$ of the energy of the incoming air was extracted. This is a correct calculation, but it only considers the incoming air which eventually travels through the rotor.

The last step in calculating the Betz efficiency Cp is to divide the calculated power extracted from the flow by a reference power. As its reference power, the Betz analysis uses the power of air upstream moving at V1 through the cross-sectional area S of the rotor. Since $A_{1}={\tfrac {2}{3}}S$ at the Betz limit, the rotor extracts ${\tfrac {8}{9}}$ of ${\tfrac {2}{3}}$ , or ${\tfrac {16}{27}},$ of the incoming kinetic energy.

Because the cross-sectional area of wind flowing through the rotor changes, there must be some flow of air in the directions perpendicular to the axis of the rotor. Any kinetic energy associated with this radial flow has no effect on the calculation because the calculation considers only the initial and final states of the air in the system.

## Upper Bounds on windmills

Although it is often touted (e.g. ) as the definitive upper bound on energy extraction by any possible windmill it is not. Despite the misleading title of his article, Betz (nor Lanchester) never made such an unconditional claim. Notably, a windmill operating at the Betz maximum efficiency has a non-zero wind velocity wake. Any actuator disk of the same or smaller diameter placed downstream of the first will extract added power from the same wind field and so the combined dual actuator complex exceeds Betz limit. The second actuator disk could be but need not be in the far field wind zone (parallel streamline) for this consideration to hold.

The reason for this surprising exception to a law based solely on energy and flux conservation laws lurks in the seemingly modest assumption of transverse uniformity of the axial wind profile within the stream lines. For example, the aforementioned dual actuator windmill has,downstream, a transverse wind profile that has two distinct velocities and thus is not bound by the limits of the single actuator disk.

Mathematically, the derivation for an single actuator disk implicitly embeds the assumption that the wind does not change velocity as it transits the "infinitely thin" actuator; in contrast, in the dual actuator hybrid, the wind does change velocity as it transits, invalidating the derivation's key step requiring constant velocity. A single infinitely thin actuator cannot change the velocity because it would otherwise not conserve flux, but in the hybrid pair, flux can be shed (outside the crossection) between the actuators allowing a different final outlet velocity than the inlet velocity.

Physical multi-coaxial-rotor windmills have been analyzed. Although these do not exceeded Betz limit in practice, this may be attributable to the fact that rotors not only have losses but must also obey angular momentum and the Blade element momentum theory which limits their efficiency below Betz limit.

## Economic relevance

Most real windmills are aerodynamically "thin" making them approximate the assumptions of Betz law. To the extent that a typical windmill approximates the assumptions in Betz law, then Betz limit places an approximate upper bound on the annual energy that can be extracted at a site. Even if a hypothetical wind blew consistently for a full year, any windmill well approximated by the actuator disk model can extract no more than the Betz limit of the energy contained in that year's wind could be extracted.

Essentially increasing system economic efficiency results from increased production per unit, measured per square meter of vane exposure. An increase in system efficiency is required to bring down the cost of electrical power production. Efficiency increases may be the result of engineering of the wind capture devices, such as the configuration and dynamics of wind turbines, that may increase the power generation from these systems within the Betz limit. System efficiency increases in power application, transmission or storage may also contribute to a lower cost of power per unit.

## Points of interest

The assumptions of the Betz derivation impose some physical restrictions on the nature of windmills it applies to (identical inlet/outlet velocity for example). But beyond those assumptions, the Betz limit has no dependence on the internal mechanics of the wind extraction system, therefore S may take any form provided that the flow travels from the entrance to the control volume to the exit, and the control volume has uniform entry and exit velocities. Any extraneous effects can only decrease the performance of the system (usually a turbine) since this analysis was idealized to disregard friction. Any non-ideal effects would detract from the energy available in the incoming fluid, lowering the overall efficiency.

Some manufacturers and inventors have made claims of exceeding the limit by using nozzles and other wind diversion devices, usually by misrepresenting the Betz limit and calculating only the rotor area and not the total input of air contributing to the wind energy extracted from the system.

The Betz limit has no relevance when calculating turbine efficiency in a mobile application such as a wind-powered vehicle, as here the efficiency could theoretically approach 100% minus blade losses if the fluid flow through the turbine disc (or equivalent) were only retarded imperceptibly. As this would require an infinitely large structure, practical devices rarely achieve 90% or over. The amount of power extracted from the fluid flow at high turbine efficiencies is less than the Betz limit, which is not the same type of efficiency.[citation needed]

## Modern development

In 1934 H. Glauert derived the expression for turbine efficiency, when the angular component of velocity is taken into account, by applying an energy balance across the rotor plane. Due to the Glauert model, efficiency is below the Betz limit, and asymptotically approaches this limit when the tip speed ratio goes to infinity.

In 2001, Gorban, Gorlov and Silantyev introduced an exactly solvable model (GGS), that considers non-uniform pressure distribution and curvilinear flow across the turbine plane (issues not included in the Betz approach). They utilized and modified the Kirchhoff model, which describes the turbulent wake behind the actuator as the "degenerated" flow and uses the Euler equation outside the degenerate area. The GGS model predicts that peak efficiency is achieved when the flow through the turbine is approximately 61% of the total flow which is very similar to the Betz result of 23 for a flow resulting in peak efficiency, but the GGS predicted that the peak efficiency itself is much smaller: 30.1%.

In 2008, viscous computations based on computational fluid dynamics (CFD) were applied to wind turbine modeling and demonstrated satisfactory agreement with experiment. Computed optimal efficiency is, typically, between the Betz limit and the GGS solution.