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is the non‐dimensional CPλ curve, and the performance curve under fixed‐pitch conditions for a typical three bladed turbine of the type used for large‐scale generation of electrical power is shown in Figure 3.50.

      The first point to notice is that the maximum value of CP is only 0.47, achieved at a tip speed ratio of 7, which is much less than the Betz limit for that tip speed ratio. The discrepancy is caused, in this case, by drag and tip‐losses, but the stall also reduces the CP at low values of the tip speed ratio.

Graph depicts the C P - λ performance curve for a modern three blade turbine. Graph depicts the C P - λ performance curve for a modern three blade turbine showing losses.

      3.12.3 The effect of solidity on performance

      The solidity could also have been changed by changing the blade chord.

      The main effects to observe of changing solidity are:

      1 Low solidity produces a broad, flat curve, which means that the CP will change very little over a wide tip speed ratio range, but the maximum CP is low because the drag losses are high (drag losses are roughly proportional to the cube of the tip speed ratio).

      2 High solidity produces a narrow performance curve with a sharp peak, making the turbine very sensitive to tip speed ratio changes and, if the solidity is too high, has a relatively low maximum CP. The reduction in CP max is caused by stall losses.

      3 An optimum solidity appears to be achieved with three blades, but two blades might be an acceptable alternative because although the maximum CP is a little lower, the spread of the peak is wider, and that might result in a larger energy capture.

      It might be argued that a good solution would be to have a large number of blades of small individual solidity, but this greatly increases production costs and results in blades that are structurally weak and very flexible.

Graph depicts the effect of changing solidity.

      3.12.4 The CQλ curve

      The torque coefficient is derived from the power coefficient simply by dividing by the tip speed ratio, and so it does not give any additional information about the turbine's performance. The principal use of the CQλ curve is for torque assessment purposes when the rotor is connected to a gearbox and generator.

      The peak of the torque curve is at the stall onset and occurs at a lower tip speed ratio than the peak of the power curve.

      3.12.5 The CTλ curve

      The thrust force on the rotor is directly applied to the tower on which the rotor is supported and so considerably influences the structural design of the tower.

Graph depicts the effect of solidity on torque. Graph depicts the effect of solidity on thrust.

      3.13.1 Introduction

      The majority of wind turbines currently installed generate electricity. Whether or not these turbines are grid connected, they need to produce an electricity supply that is of constant frequency else many common appliances will not function properly. Consequently, a mode favoured in the early years of wind turbine development has been operation at constant rotational speed. Connected to the grid a constant‐speed turbine is automatically controlled, whereas a stand‐alone machine needs to have speed control and a means of dumping excess power.

      3.13.2 The KP−1/λ curve

      An alternative performance curve can be produced for a turbine controlled at constant speed. The CP –λ curve shows, non‐dimensionally, how the power would vary with rotational speed if the wind speed was held constant. The KP –1/λ curve describes, again non‐dimensionally, how the power would change with wind speed when constant rotational speed is enforced. KP is defined as

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