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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

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