Page 19 - Wind Energy Handbook
P. 19

LIST OF SYMBOLS                                                         xix


             K P         power coefficient based on tip speed
             K SMB       size reduction factor accounting for the lack of correlation of wind
                         fluctuations over structural element or elements
             K Sx (n 1 )  size reduction factor accounting for the lack of correlation of wind
                         fluctuations at resonant frequency over structural element or elements
             K í ( )     modified Bessel function of the second kind and order í
             K(÷)        function determining the induced velocity normal to the plane of a
                         yawed rotor
             L           length scale for turbulence (subscripts and superscripts according to
                         context); lift force
             L x u       integral length scale for the along wind turbulence component, u,
                         measured in the longitudinal direction, x
             m           mass per unit length, integer
                         generalized mass with respect to the ith mode
             m i
                         generalized mass of tower, nacelle and rotor with respect to tower
             m T1
                         first mode
             M           moment; integer
             M           mean bending moment
                         teeter moment
             M T
                         blade in-plane moment (i.e., moment causing bending in plane of
             M X
                         rotation); tower side-to-side moment
             M Y         blade out-of-plane moment (i.e., moment causing bending out of
                         plane of rotation); tower fore-aft moment
             M Z         blade torsional moment; tower torsional moment
             M YS        low-speed shaft moment about rotating axis perpendicular to axis of
                         blade 1
             M ZS        low-speed shaft moment about rotating axis parallel to axis of blade 1
             M Y N       moment exerted by low-speed shaft on nacelle about (horizontal) y-
                         axis
             M Z N       moment exerted by low-speed shaft on nacelle about (vertical) z-axis
             n           frequency (Hz); number of fatigue loading cycles; integer
             n 0         zero up-crossing frequency of quasistatic response
             n 1         frequency (Hz) of 1st mode of vibration
             N           number of blades; number of time steps per revolution; integer
             N(r)        centrifugal force
             N(S)        number of fatigue cycles to failure at stress level S
             p           static pressure
             P           aerodynamic power; electrical real (active) power
              m
             P ( )       associated Legrendre polynomial of the first kind
              n
             q(r, t)     fluctuating aerodynamic lift per unit length
             Q           rotor torque; electrical reactive power
                         aerodynamic torque
             Q a
              _
             Q Q         rate of heat flow
             Q           mean aerodynamic lift per unit length
             Q D         dynamic factor defined as ratio of extreme moment to gust quasistatic
                         moment
             Q g         load torque at generator
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