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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 />
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