Abstract
This study presents a unified modeling framework for unconventional horizontal axis wind turbines (HAWTs) that utilize axially extended, non-radial blade geometries. Recent bio-inspired and helical designs have reported performance levels that are difficult to interpret within the standard single-plane actuator-disc framework: they overcome the classical Betz limit which is derived for an ideal single rotor operating under one-dimensional axial-flow assumptions. To address this gap in the technology description, we introduce the Generalized Multi-Stage Actuator Disc Model, which discretizes the rotor into a sequence of interacting aerodynamic stages aligned with the flow axis. We rigorously evaluate four topological configurations, Solid Divergent, Hollow Divergent, Solid Convergent, and Hollow Convergent, using numerical optimization to determine their theoretical performance limits. Our results show that all multi-stage configurations converge to a maximum theoretical efficiency of
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