1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
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38<br />
<strong>1.</strong> MAGNETIC CONFINEMENT<br />
<strong>1.</strong>2 FTU Facilities<br />
components may rise simultaneously<br />
if the non-locality of the measurement<br />
is taken into account, since it<br />
integrates the low frequency at some<br />
outer radial zone. It is also important<br />
that the low-frequency rotation<br />
remain unchanged. It is worth noting<br />
that the quasi-coherent rotation is<br />
sensitive to gradients, whereas the<br />
low-frequency is closer to that of the<br />
bulk plasma. Figure <strong>1.</strong>33 shows the<br />
evolution of some turbulence<br />
parameters in an experiment with the<br />
injection of four deuterium pellets<br />
[<strong>1.</strong>50]. The discharge has I p =<strong>1.</strong>2 MA<br />
and B t =7.9 T. The probing Xl mode<br />
was used with a cut-off density of<br />
2.76×10 20 m -3 . The trace of the<br />
reflected wave amplitude (fig. <strong>1.</strong>33b)<br />
shows that reflection appears just<br />
transiently after the first pellet at<br />
t=800 ms and becomes permanent<br />
after injection of the second. This is<br />
eV/cm 104 s-1 Part in signal cm a.u. 1019 m-3<br />
ω rotation<br />
pellets<br />
Electron density<br />
Reflection radius<br />
Broad band<br />
Low frequency<br />
the first time that poloidal correlation measurements in the Xl mode have been<br />
carried out in tokamaks, with the antennas located at the low-field side and the<br />
poloidal angle 17.5° above the equatorial plane. Such geometry results in a<br />
significant deviation of the incident wave from the perpendicular direction, due to<br />
the dependence of the refractive index on the <strong>magnetic</strong> field and on the Shafranov<br />
shift of the plasma column. This makes it impossible to measure reflections close to<br />
the centre of a plasma with a flat density profile. Thus, reliable results can be<br />
obtained only when the amplitude of the reflected wave is larger than some<br />
minimum value, as shown in figure <strong>1.</strong>33b. The most distinctive feature is the drop of<br />
the quasi-coherent rotation velocity after the second pellet. An explanation for this<br />
could be that the reflection layer gradually moves towards the central region where<br />
the gradients are smaller due to density decay. At the same time, the low-frequency<br />
component rotates more slowly and does not show any strong variation in time. This<br />
may indicate again that this component is related to plasma rotation, whereas the<br />
quasi-coherent one depends on gradients. The simultaneous suppression of both<br />
components in the central region, as observed in these experiments, suggests a<br />
physical relation between these turbulence features and also the presence of a good<br />
<strong>confinement</strong> zone near the centre.<br />
The fully non-inductive discharges with LHCD [<strong>1.</strong>51] make it possible to reveal the<br />
fine structure of quasi-coherent turbulence. In figure <strong>1.</strong>34 the usually smooth spectral<br />
maxima of these fluctuations split into an envelope of five peaks with a 3.1-kHz<br />
spacing in frequency. The depth of amplitude modulation shows that only the quasicoherent<br />
fluctuations are 100% modulated whereas the broadband are not. This<br />
supports the idea that the two components have different underlying physical<br />
mechanisms. Poloidal correlation measurements during the same time slice give the<br />
rotation velocity and show that the mean m number is equal to 48. Thus, the 3.1-kHz<br />
frequency step corresponds to an m number increment of three instead of one. In<br />
order to solve this problem, consider the reflection from a plasma region with a flat<br />
current profile around the q=3 surface but with a rather steep density gradient. The<br />
modes with m/n ≠3 will be far away from the reflection layer and will not be “seen”<br />
by the reflectometer. Thus, only modes with an m increment of three will be<br />
observed, in accordance with experimental data. Analysis of the bursting of the<br />
4<br />
2<br />
20<br />
10<br />
0<br />
20<br />
10<br />
0<br />
0.5<br />
0.0<br />
0.2<br />
0.0<br />
<strong>1.</strong>0<br />
0.5<br />
0.0<br />
m=2 HF<br />
Signal amplitude<br />
Reliability level<br />
LF<br />
100<br />
0 dT/dr<br />
700 800 900 1000 1100 1200<br />
Time (ms)<br />
Fig. <strong>1.</strong>33 - Evolution of<br />
turbulence behaviour<br />
during a high-<strong>confinement</strong><br />
phase of a pellet-fuelled<br />
discharge.<br />
[<strong>1.</strong>50] V. Pericoli Ridolfini<br />
et al. , Phys. Rev. Lett. ,<br />
82, 93 (1999)<br />
[<strong>1.</strong>51] S. Cirant et al.,<br />
Mode coupling trigger of<br />
tering mides in ECV<br />
heated discharges in FTU,<br />
presented at the 18 th<br />
IAEA Conference,<br />
(Sorrento 2000), paper<br />
IAEA-CN-77/EX3/3