4. Blade bending moments are being measured on a research wind turbine on a day in which the wind speed at the hub height is 9.0 m/s. A wind shear results in higher wind speed of 12.0 m/s at the top of the blade tip path and lower wind speeds of 6.0 m/s at the bottom of the blade tip path. A wind direction change results in a cross-wind of 0.60 m/s. The 24 m. diameter tur- bine starts with a flap hinge angle, Bo = 0.05 radians and, at the moment that measurements of are being made, the rate of change of the flap hinge angle is %3D = 0.01 rad/s. %3D

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Chapter6: Forced Convection Over Exterior Surfaces
Section: Chapter Questions
Problem 6.34P
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4. Blade bending moments are being measured on a research wind turbine on
a day in which the wind speed at the hub height is 9.0 m/s. A wind shear
results in higher wind speed of 12.0 m/s at the top of the blade tip path and
lower wind speeds of 6.0 m/s at the bottom of the blade tip path. A wind
direction change results in a cross-wind of 0.60 m/s. The 24 m. diameter tur-
bine starts with a flap hinge angle, Bo = 0.05 radians and, at the moment that
measurements of are being made, the rate of change of the flap hinge angle is
dB1s/dt = 0.01 rad/s.
%3D
The rotor has a fixed rotation rate of 2 = 0.159s-1 (or a frequency of
1 hz.) and is 3.05 m/s from the yaw axis (bearing support). The blade pitch
angle is 0ep
= 0.05 radians (2.86°).
1. Describe how the blade angle of attack would vary during one complete
rotor revolution.
2. List all of the effects these conditions have on the load on the bearing.
3. Estimate the load due to the yawing motion of the rotor.
Transcribed Image Text:4. Blade bending moments are being measured on a research wind turbine on a day in which the wind speed at the hub height is 9.0 m/s. A wind shear results in higher wind speed of 12.0 m/s at the top of the blade tip path and lower wind speeds of 6.0 m/s at the bottom of the blade tip path. A wind direction change results in a cross-wind of 0.60 m/s. The 24 m. diameter tur- bine starts with a flap hinge angle, Bo = 0.05 radians and, at the moment that measurements of are being made, the rate of change of the flap hinge angle is dB1s/dt = 0.01 rad/s. %3D The rotor has a fixed rotation rate of 2 = 0.159s-1 (or a frequency of 1 hz.) and is 3.05 m/s from the yaw axis (bearing support). The blade pitch angle is 0ep = 0.05 radians (2.86°). 1. Describe how the blade angle of attack would vary during one complete rotor revolution. 2. List all of the effects these conditions have on the load on the bearing. 3. Estimate the load due to the yawing motion of the rotor.
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