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Analysis of aerodynamic load on straight-bladed vertical axis wind turbine

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Abstract

This paper presents a wind tunnel experiment for the evaluation of energy performance and aerodynamic forces acting on a small straight-bladed vertical axis wind turbine (VAWT) depending on several values of tip speed ratio. In the present study, the wind turbine is a four-bladed VAWT. The test airfoil of blade is symmetry airfoil (NACA0021) with 32 pressure ports used for the pressure measurements on blade surface. Based on the pressure distributions which are acted on the surface of rotor blade measured during rotation by multiport pressure-scanner mounted on a hub, the power, tangential force, lift and drag coefficients which are obtained by pressure distribution are discussed as a function of azimuthally position. And then, the loads which are applied to the entire wind turbine are compared with the experiment data of pressure distribution. As a result, it is clarified that aerodynamic forces take maximum value when the blade is moving to upstream side, and become small and smooth at downstream side. The power and torque coefficients which are based on the pressure distribution are larger than that by torque meter.

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Abbreviations

A :

cross-sectional area (m2)

c :

blade chord length (m)

C N :

normal force coefficient on blade

C D :

drag coefficient on blade

C L :

lift coefficient on blade

C lateral :

lateral force coefficient on rotor

C p :

pressure coefficient

Cpower :

power coefficient

C Q :

torque coefficient on rotor

C thrust :

thrust coefficient on rotor

C T :

tangential force coefficient on blade

D :

rotor diameter (m)

F D :

drag force on blade (N)

F L :

lift force on blade (N)

F N :

normal force on blade (N) Greek letters

F T :

tangential force on blade (N)

H :

height of rotor (m)

i :

measurement point position

N :

number of blades

p:

pressure on blade surface (Pa)

P:

power absorbed from wind (W)

P d :

power for downstream (W)

P u :

power for upstream (W)

pi :

pressure at measurement tap (Pa)

p 0 :

reference static pressure (Pa)

R:

rotor radius (m)

Re :

local Reynolds number

Si :

measurement taps distance connecting midpoint of pressure measurement tap adjacent to each other in airfoil section (m)

Q :

rotor torque (N·m)

U 0 :

mainstream wind velocity (m/s)

V :

tip speed of blade (m/s)

W :

relative flow velocity (m/s)

x :

longitudinal coordinate (m)

y :

lateral coordinate (m)

Δy :

a minute width in y-axis direction (m)

z :

vertical coordinate (m)

α:

angle of attack (deg)

β:

blade pitch angle (deg)

θ:

azimuth angle (deg)

γ:

inclination angle of pressure measurement taps in position of i (deg)

λ:

tip speed ratio

ν:

kinematic viscosity (m2/s)

ρ:

air density (kg/m3)

φ :

angle of resultant flow velocity (deg)

ω:

angular velocity of rotor (1/s)

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Li, Q., Maeda, T., Kamada, Y. et al. Analysis of aerodynamic load on straight-bladed vertical axis wind turbine. J. Therm. Sci. 23, 315–324 (2014). https://doi.org/10.1007/s11630-014-0712-8

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  • DOI: https://doi.org/10.1007/s11630-014-0712-8

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