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FYS200, Assignment 2 Diana Quintero Castro 19 October 2021 Consider the adiabatic wind turbine, shown in the figure below, within the following assumptions: Poo Pi pressures 0 : velocities*É 0*0*8 A :...

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FYS200, Assignment 2
Diana Quintero Castro
19 October 2021
Consider the adiabatic wind tu
ine, shown in the figure below, within the
following assumptions:
Poo Pi pressures
0 : velocities*É 0*0*8 A : Areas -
gild
Poo
Ad Aw
No
Aoo
wakeful
Upstream lad
• The flow is steady and the fluid is incompressible.
• The flow is uniform through the disc and in the wake.
• The stream is horizontal.
• The actuator disc models the tu
ine blades and the disc extracts energy
from the flow.
• The actuator disc creates a pressure discontinuity across the disc (P+,
P−).
• The disc does not impart any swirl to the flow.
1. Write a short introduction explaining how wind tu
ines produce electric-
ity (include due references).
2. Write the continuity equation for the three relevant points highlighted in
the sketches (far stream: ∞, at the actuator disc: d and in the wake: w.)
3. Write the Bernoulli equation for the top and the bottom stream lines
(green lines in the sketch).
1
4. Calculate the change in the momentum rate (∆ṗ = Ṁ∆v ) at the actuato
disc, consider the velocity at the disc as an average velocity with the form
vd =
1
2
(vinf + vw)
Rewrite the momentum rate as a function of the axial induction factor,
defined as:
a =
vinf − vd
vinf
5. The force causing this change in momentum rate comes from the pressure
difference across the actuator disc (P+, P−), as
Force = change in momentum rate = change in pressure× actuator area
Use the equations found above to rewrite the force equation.
6. Use the expression above to find a relation between the speed in the wake
and in the far stream.
7. Calculate the power output as
Power = Force× velocity at the disc
and plot the power as a function of a (you can use a plotting program fo
that eg. mathematica, matlab).
8. Calculate the power coefficient as
Cpow =
Powe
Power of wind in a free stream
where
Power of wind in a free stream =
1
2
ρv3infAd
Find for which value of a the power coefficient has a maximum. This
maximum is called the Betz limit.
9. Calculate the enthalpy change in this process for amax.
10. Write a short discussion of your results and conclusions, for example,
discuss in which settings the power output can be increased, e.g. down by
the sea, up in a mountain, etc.
In order to pass this assignment, you will need to answer co
ectly at least
50% of the questions above. Deadline: 9th November 2021.
2
Answered 4 days After Oct 27, 2021

Solution

Amar Kumar answered on Nov 01 2021
131 Votes
FYS200, Assignment 2
Diana Quintero Castro
19 October 2021
Consider the adiabatic wind tu
ine, shown in the figure below, within the following assumptions:
    *É 0*0*8Poo    Pi press::    ures
0 velocities
A Areas -
gild
Poo
    Ad    Aw
No wakeful
Aoo
Upstream lad
· The flow is steady and the fluid is incompressible.
· The flow is uniform through the disc and in the wake.
· The stream is horizontal.
· The actuator disc models the tu
ine blades and the disc extracts energy from the flow.
· The actuator disc creates a pressure discontinuity across the disc (P+, P−).
· The disc does not impart any swirl to the flow.
1. Write a short introduction explaining how wind tu
ines produce electricity (include due references).
The streamlined power of the rotor sharp edges, which act likewise to a plane wing or helicopter rotor edge, changes over wind energy into power in a
eeze tu
ine. The gaseous tension on one side of the edge
ings down when wind blows across it. Lift and drag are made by the distinction in gaseous tension across the different sides of the edge. The lift power is more noteworthy than the drag power, making the rotor turn. The rotor is associated with the generator either straightforwardly or by a shaft and a progression of cog wheels that permit the generator to be genuinely more modest by accelerating the twist. The change of streamlined power to generator revolution produces electricity.
2. Write the continuity equation for the three relevant points highlighted in the sketches (far stream: ∞, at the actuator disc: d and in the wake: w.)
3. Write the Bernoulli equation for the top and the bottom streamlines (green lines in the sketch).
Bernoulli’s equation
4. Calculate the change in the...
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