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    AAE 415 Aerodynamic Design

    Final Project Presentation

    Large Horizontal-Axis

    Wind Turbine DesignTed Light

    Jeff Robinson

    December 13, 2003

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    Outline

    Background

    Wind Energy & History

    Types of Wind Turbines

    Wind Turbine Aerodynamics

    Design Process

    Starting Point and Analysis Method

    Results

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    Wind Energy & History

    Wind energy has been used

    for thousands of years, for

    sailing, pumping water,

    grinding grain, etc.

    In the early 1900s, windturbines were used to

    produce direct electric

    current to small areas

    Oil Crisis of 1970s renewedinterest in wind turbines as a

    cheap, clean, unlimited

    source of energy

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    Types of Wind Turbines

    Darrius VerticalAxis Wind Turbine

    Large HorizontalAxis Wind Turbine

    Traditional Windmill

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    Airfoil Aerodynamics

    Wind = V0

    Rotation = r*W

    Relative Wind = W a

    Wind Speed and Turbine Rotation must be

    combined to find total velocity that airfoil sectionssee

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    Desired Airfoil Qualities

    For a fixed-pitch, constant speed machine,

    recommended airfoil qualities at 0.75R are:

    High L/D

    Low clmax near tip reduces tendency to

    overpower generator in high wind speeds

    Insensitive to surface roughness (bugs, birds,

    bullets)

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    Design Process

    CMARC used to analyze designs

    Existing wind turbine with known geometry

    and performance modeled for baseline

    comparison

    Assumed constant velocity generator

    (Power) = (Moment)*(Rotation Rate)

    Variation and Analysis of Designs

    Geometric parameters modified

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    Analysis Strategy

    Start with an existing wind turbine, then

    modify its geometry

    Geometry varied

    Airfoil section

    Twist distribution

    Chord distribution

    Rotational rate, number of blades and

    span were held constant

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    Mod-2 Wind Turbine

    Manufactured by Boeing in late 1970s

    Development sponsored by NASA

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    Mod-2 Wind Turbine Specifications

    3.45 m 1.43 m

    13.7 m

    45.7 m

    Diameter = 91.4 m

    No. of Blades = 2 Average Wind Speed = 12.5 m/s

    Rotation Rate = 17.5 rpm

    Airfoil: NACA 23024

    Power Output = 2.5 MW

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    CMARC Inputs

    Rotation rate about x-axis set to that of

    Mod-2 wind turbine (17.5 rpm)

    Many wind turbines are constant speed

    Wind Speed set to local average wind

    speed for Mod-2 (12.5 m/s)

    Baseline geometry emulated Mod-2

    geometry, then varied

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    Results

    r/R (1) (2) (3)

    0 15 14 10

    0.25 11.4 11.4 8

    0.5 5.7 7 6

    0.75 3.8 3.8 4

    1 2.85 2.85 2

    Chord Changes

    r/R (1) (2) (3)

    0 6.1 6.0 5.5

    0.25 66.7 27.8 83.5

    0.5 83.4 49.5 89

    0.75 93.8 71.3 90

    1 111.6 93.0 92

    Twist Changes (values in deg from wind axis)

    Mod-2 Baseline Model 5816 ---

    Mod-A Airfoil Changed to NACA 651-012 5516 -12%

    Mod-B Airfoil Changed to NACA 65-410 6179 15%

    Mod-C Airfoil Changed to Althaus AH 93-W-145 2551 -131%

    Mod-D Chord Change (1) from Mod-B with no sweep 8914 124%

    Mod-E Chord Change (2) from Mod-B with no sweep 8442 105%

    Mod-F Chord Change (3) from Mod-B with no sweep 7872 82%

    Mod-G Chord Change (3) from Mod-B with sweep 9380 143%

    Mod-H Twist Change (1) from Mod-G 10367 182%

    Mod-I Twist Change (2) from Mod-G 7849 81%

    Mod-J Twist Change (3) from Mod-G 7735 77%

    Mod-2 Rating Published Power Rating 2500

    Model # DescriptionPower (kW)

    Dfrom

    Baseline

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    Results

    Leading Edge

    Root Section

    Blade Tip

    Airfoil NACA 65-410

    r/R Chord (m) Twist (deg)0 10 6.1

    0.25 8 66.7

    0.5 6 83.4

    0.75 4 93.8

    1 2 111.6

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    Cp Distribution

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    Wake

    for

    Best

    Blade

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    Results

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    Questions?