I T HAS long been known that the popular and useful controlvolume actuator-disk model for wind turbines encounters a troublesome behavior as the thrust coefficient for the rotor/disk approaches 1, which occurs when the velocity at the rotor/disk approaches half that of the freestream level and the axial velocity at the downstream outlet approaches zero. This is discussed in detail in nearly all texts and papers involving wind turbines (as, for example, in [1–8]). Beyond a thrust-coefficient value of 1, it is well understood that the current version of the model does not apply, because it predicts flow entering the control volume at the downstream outlet, thus negating its further use and leaving a gap in the theory for an important range of the controlling parameters. To date, this gap has been addressed largely with either empirical expressions and/or computational fluid dynamics (CFD) methods. Based on Glauert’s 1926 analysis of data taken for windmilling helicopter blades in open-jet wind tunnels (as discussed in [1]) and its adaption to wind turbines by Stoddard [5], it is now widely accepted that the classical model begins to break down somewhere near a rotor/disk velocity ratio of 0.6 (induction factor of 0.4). For larger induction factors, it is assumed that a turbulent-wake state ensues, with reverse and/or unsteady flow effects dominating the flow as the rotor/disk velocity further reduces to zero: i.e., the rotor/disk stalls. It is further widely accepted that Glauert’s empirical expression for the rotor/disk performance prevails in this turbulent-wake region, with several attempts at improving its utility, as summarized by Buhl [8]. Additionally, recent CFD studies by Sorensen et al. [6] andMikkelsen [7] appear to reinforce this empirical model. Recently, however, two studies [9,10] using control-volume actuator-disk modeling of wind-tunnel blockage influences on rotor/ disk performance uncovered an entirely new family of well-behaved steady-state solutions that exist in the turbulent-wake parameter space: i.e., for induction factors from 0.4 all the way to 1. Moreover, the results of [9] implied the existence of a new well-behaved solution family for induction factors above 0.5, even for the zeroblockage condition. The current work provides this new exact solution for induction factors from 0.5 to 1 based on a limit-analysis solution of the control-volume actuator-disk equations. This new solution provides the heretofore missing piece of the basic theory, filling the gap for induction factors of 0.5 to 1. Comparisons of the new analytical solutions with experiments and CFD studies of actuator disks provide strong evidence of its validity. The relevance of the results to CFD modeling, wind-tunnel testing, and/or field testing of wind turbines is discussed.
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