Gyrofluid simulation on the nonlinear excitation and radial structure of geodesic acoustic modes in ITG turbulence

The nonlinear excitation and saturation mechanism of geodesic acoustic mode (GAM), as well as its radial structure, in tokamak plasmas are investigated by applying a newly well-benchmarked gyrofluid model. At first, an empirical closure relation for the conventional three-field gyrofluid modeling is...

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Bibliographic Details
Published in:Journal of physics. Conference series 2008-07, Vol.123 (1), p.012027
Main Authors: Li, J Q, Kishimoto, Y, Miyato, N, Miki, K, Anderson, J, Shi, B R
Format: Article
Language:English
Subjects:
Excitation
Flow stability
Ion temperature
Landau damping
Physics
Plasmas (physics)
Reynolds stress
Sound waves
Turbulence
Zonal flow (meteorology)
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Summary:The nonlinear excitation and saturation mechanism of geodesic acoustic mode (GAM), as well as its radial structure, in tokamak plasmas are investigated by applying a newly well-benchmarked gyrofluid model. At first, an empirical closure relation for the conventional three-field gyrofluid modeling is presented for ion temperature gradient (ITG) fluctuations and the GAMs. The zonal flow damping is precisely examined by comparing with theoretical predictions and other kinetic calculations. Then, a local code and the global version are advanced to simulate the nonlinear excitation of the GAMs by ITG fluctuations through the Reynolds stress. It is found that the GAM instability can be nonlinearly excited under the competition between the nonlinear driving and the collisionless damping. The pump amplitude threshold of the GAM instability is higher than that of the zonal flow instability. Meanwhile, the unstable GAMs are mainly saturated by the intrinsic Landau damping, which is different from the stationary zonal flow counterpart. It is testified that the sound waves are damped fluctuations in ITG turbulence. Furthermore, the radial structure of the GAMs is shown as krρi ≤ 1.0, which is shorter than that of the pure zonal flows.
ISSN:1742-6596
1742-6588
1742-6596
DOI:10.1088/1742-6596/123/1/012027