Surface-Layer Wind and Turbulence profiling from LIDAR: Theory ...
Surface-Layer Wind and Turbulence profiling from LIDAR: Theory ...
Surface-Layer Wind and Turbulence profiling from LIDAR: Theory ...
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Altitude [m]<br />
Length of the<br />
beam, p’[m]<br />
Diameter of<br />
scanning cone<br />
[m]<br />
40m 43.88m 44.77m<br />
60m 66.97m 68.18m<br />
80m 90.07m 91.70m<br />
100m 113.16m 115.21m<br />
200m 228.64m 232.77m<br />
against the direction of the wind, maximum Doppler shifts<br />
occur, see. Figure 3.<br />
Tabel 1: Geometrical characteristics of the conical scans<br />
The Doppler shift results <strong>from</strong> the difference of the wave<br />
vector k r e<br />
for the emission <strong>and</strong> k r r<br />
for the reflection. Let B r<br />
be the propagation vector of the transmitted Laser beam:<br />
Fig. 3:30minute of raw wind measurements obtained <strong>from</strong><br />
Doppler shifts as function of conical scan angle [0; 2π].<br />
In Fig. 3 the observed Doppler shifts have been transformed<br />
into velocities by the following equation:<br />
st ( , ) = ut ( )cos( − )sin( Φ ) + wt ( )cos( Φ)<br />
(3)<br />
θ θ θ<br />
d<br />
Fig. 2: Details of the interaction between the laser radiation<br />
<strong>and</strong> the horizontal component of the wind<br />
The mean wind direction is aligned along the xaxis:<br />
r µ ≡ u<br />
r ,<br />
r r<br />
v = w= 0<br />
r<br />
. To calculate the resulting Doppler shift, we<br />
define two frequencies, one representing the emission of the<br />
signal, <strong>and</strong> one representing its reception:<br />
r r ⎛ u<br />
⎞<br />
ω' e<br />
= ω<br />
0<br />
+ ke. µ ⇔ ν '<br />
e<br />
= ν ⎜1− cos( θ)sin( Φ)<br />
⎟<br />
⎝ c<br />
⎠<br />
(1)<br />
r r ⎛ u<br />
⎞<br />
ω' r<br />
= ω<br />
0<br />
+ kr. µ ⇔ ν '<br />
r<br />
= ν ⎜1+ cos( θ)sin( Φ)<br />
⎟<br />
⎝ c<br />
⎠<br />
where ν is the frequency [Hz]. The modulus of wave vector is<br />
r 2πν<br />
defined as k = . The Doppler shift of an elastic<br />
c<br />
scattered photon results as the difference between the outgoing<br />
<strong>and</strong> the backscattered radiation:<br />
u<br />
∆ ν = ν '<br />
r− ν '<br />
e<br />
= 2 ν cos( θ)sin( Φ ) (2)<br />
c<br />
This represents the Doppler shift detected by the Lidar. The<br />
quantity is the angle between the aerosol transported by the<br />
wind <strong>and</strong> the beam. When /2 or 3/2, the Doppler shift is<br />
zero. The ideal cases are =0 or ; but due to the conical<br />
scanning at fixed angle to vertical there will always be nonzero<br />
Doppler shifts wherever the wind comes <strong>from</strong>. The<br />
Doppler shift frequency signal that appears on the Lidar’s<br />
detector will give the following typical picture if we sample<br />
complete rotations. When the Laser beam is pointing into or<br />
<strong>and</strong> then shown as function of scan angle . A curve has been<br />
fitted through the data points. The fitted curve allows<br />
calculation of u, w <strong>and</strong> if the Lidar has been properly<br />
oriented (to the North) a curve fit also yields the direction d<br />
of the mean wind speed. In normal operation mode the<br />
horizontal wind vector is determined <strong>from</strong> 3 full conical<br />
rotations of 1second duration each. During each revolution a<br />
total of 25 Doppler spectra are obtained with the present<br />
instrument. An average wind speed <strong>from</strong> the conical scans is<br />
then obtained by a curve fit to 3 full rotations of such Doppler<br />
measurements <strong>and</strong> encompasses therefore up to 75 raw<br />
spectra as obtained over three revolutions of 2. u(t), w(t) <strong>and</strong><br />
d are consequently representing averages over 3 seconds in<br />
time.<br />
Geometry of the Gaussian beam:<br />
The radius <strong>and</strong> the focal width of the Laser beam changing as<br />
function of the measurement height <strong>and</strong> the effective<br />
measurement volume is consequently determined by the<br />
system optics. The laser beam is characterized by its Rayleigh<br />
length<br />
z<br />
R .<br />
2<br />
πW0<br />
z R<br />
= 50.6µ<br />
m<br />
λ<br />
At the output of the fibre this quantity is<br />
= , where W 0 is the radius of the<br />
beam in the optical fiber. This Rayleigh length represents the<br />
halfwidth where most of the power of the laser beam is<br />
gathered, according to the Lorentzian distribution of energy<br />
among the beam. By adjusting the fiber end near the focal<br />
point of the lens, the beam can be focused to take wind<br />
measurements at preset heights. The characteristics of the<br />
laser beam at the fiber end is via the lens projected to the<br />
external focal volume of length z (Rayleigh length) <strong>and</strong> of<br />
focal width W. At a distance p’<strong>from</strong> the lens the beams crosssection<br />
is given by 1 :<br />
R