Abstract

Abstract. The design of a ducted wind turbine modeled using an actuator disc was studied using Reynolds-averaged Navier–Stokes (RANS) computational fluid dynamics (CFD) simulations. The design variables included the rotor thrust coefficient, the angle of attack of the duct cross section, the radial gap between the rotor and the duct, and the axial location of the rotor in the duct. Two different power coefficients, the rotor power coefficient (based on the rotor swept area) and the total power coefficient (based on the exit area of the duct), were used as optimization objectives. The optimal value of thrust coefficients for all designs was nearly constant, having a value between 0.9 and 1. The rotor power coefficient was sensitive to rotor gap but was insensitive to the rotor's axial location for positions ranging from upstream of the throat to nearly half the distance down the duct. Compared to the design that maximized rotor power coefficient, the design for maximal total power coefficient was characterized by a smaller angle of attack, a smaller rotor gap, and a downstream placement of the rotor. The insensitivity of power output to the rotor position implies that a rotor placed further downstream in the duct could produce the same power with a considerably smaller duct exit area and thus a greater total power coefficient. The design for that maximized total power coefficient exceeded Betz's limit with a total power coefficient of 0.67.

Highlights

  • A properly designed duct placed around a wind turbine can increase power output by increasing the mass flow rate through the rotor

  • Ducted wind turbines (DWTs) are called diffuser-augmented wind turbines (DAWT) or shrouded wind turbines. (Lilley and Rainbird, 1956) performed a one-dimensional momentum analysis of DWTs and concluded that higher expansion ratios of the duct and more subatmospheric pressures at the exit plane of the duct result in higher power outputs

  • The optimal design of a ducted wind turbine characterized by the thrust coefficient of the rotor CT, rotor, the angle of attack of the duct cross section α, the rotor gap r/D, and the axial location of the rotor z/c was investigated

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Summary

Introduction

A properly designed duct placed around a wind turbine can increase power output by increasing the mass flow rate through the rotor. (Lilley and Rainbird, 1956) performed a one-dimensional momentum analysis of DWTs and concluded that higher expansion ratios of the duct and more subatmospheric pressures at the exit plane of the duct result in higher power outputs. They suggested wind tunnel tests with screens of different porosities to model the pressure drop across the rotor. Such experimental tests were performed by Igra (1976, 1977, 1981), Foreman et al (1978), Gilbert et al (1978), and Gilbert and Foreman (1979). As the duct can be considered an annular wing (de Vries, 1979) with higher lift, meaning more suction and circulation, high-lift airfoils were used from early experimental studies

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