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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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