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Symbol Description Unit<br />

a Axial interference factor [-]<br />

A Rotor swept area [m 2 ]<br />

a' Tangential interference factor [-]<br />

NOMENCLATURE<br />

Ab Bearing area [mm 2 ]<br />

Aproj Component area projected on to a plane perpendicular to the<br />

wind direction<br />

AS Aspect ratio [-]<br />

B Number of blades [-]<br />

c Blade chord length [m]<br />

Cd Drag coefficient [-]<br />

Cd.st Coefficient of drag at the onset of stall [-]<br />

Cf Force coefficient [-]<br />

Cl Lift coefficient [-]<br />

Cl.st Coefficient of lift at the onset of stall [-]<br />

Cp Power coefficient [-]<br />

CT Thrust coefficient [-]<br />

Cx Coefficient of tangential forces [-]<br />

Cy Coefficient of axial forces [-]<br />

D Rotor diameter [m]<br />

[m 2 ]<br />

db Bolt diameter [mm]<br />

Db Bearing diameter [mm]<br />

Dpc Bolt pitch diameter [mm]<br />

e Natural logarithm [-]<br />

E Modulus of elasticity [MPa]<br />

er Distance from centre of gravity of the rotor to the rotation axis [m]<br />

Ev Potential energy of tail [J]<br />

F Prandtl’s number [-]<br />

f� Constant [-]<br />

Fd Drag force [N]<br />

fk Characteristic material strength [MPa]<br />

Fk Characteristic capacity [N]<br />

Fl Lift force [N]<br />

FxS Axial shaft load [N]<br />

FzB Force in z direction on the blade at the blade root [N]<br />

g Acceleration due to gravity: 9.81 [m/s 2 ]<br />

G Shear modulus [MPa]<br />

GR Glide ratio [-]<br />

IB Blade mass moment of inertia about rotation axis [kg·m 2 ]<br />

K Factor [-]<br />

kmod Modification factor [-]<br />

Lfs Distance between tower flange and rotor axis [mm]<br />

107

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