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Fig. 2. Generic model of a DFIG
2.1
Aerodynamic Torque Model
Aerodynamic model involves the extraction of useful mechanical power from the
available wind power. Available wind power is given by
1
2
P
=
ρπ
R V
23
(1)
wind
, R and V are the available power in the wind, air density (kg/m 2 ),
radius of the turbine blade (m) and the wind speed (m/s) that reaches the rotor swept
area (m 2 ). The fraction of wind power that is converted to the turbine mechanical
power
where
P
,
ρ
wind
P is given by
1
(
)
P
=
ρπ
R C
2
λ β
,
V
3
(2)
m
p
2
where C gives the fraction of available wind power that is converted to turbine
mechanical power,
and
are the tip speed ratio and the pitch angle respectively.
λ
β
C , λ
The
and
β
are related by equation (3) and (4) [10]
c
c
5
(
)
2
λ
C
λ β
,
=
c
c
β
c
e
+
c
λ
(3)
i
p
1
3
4
6
λ
i
1
1
0.035
=
(4)
λ
10.08
+
β
β
2
+
1
i
c = 0.5176,
c = 116, c =0.4,
c = 5, c = 21 and
c = 0.0068 ,the relationship
Given
between
is given in figure 3.
The tip speed ratio is given by (5)
C against λ
at various
β
R
V ω
t
λ =
(5)
 
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