1995
DOI: 10.1103/physrevlett.75.645
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Direct Measurement of the Damping of Toroidicity-Induced Alfvén Eigenmodes

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Cited by 134 publications
(136 citation statements)
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“…Furthermore, in all the discharges in the alpha-heating experiment low-n NTMs were present with similar amplitudes in the low-frequency range, between ∼10 and ∼35 kHz. The triangular sweeping waveform seen in figure 9 for #42856 is the signal from the saddle coils, used to measure the damping rate of TAEs in this discharge [52]. Hence, as previously reported in [4], the presence or absence of coherent, current/pressure-driven (low-frequency) and higher frequency fast-ion driven modes can be discounted to explain the anomalous ion heating observed with the αs.…”
Section: Measurements Of the Ion And Electron Drift-wave Turbulence Smentioning
confidence: 78%
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“…Furthermore, in all the discharges in the alpha-heating experiment low-n NTMs were present with similar amplitudes in the low-frequency range, between ∼10 and ∼35 kHz. The triangular sweeping waveform seen in figure 9 for #42856 is the signal from the saddle coils, used to measure the damping rate of TAEs in this discharge [52]. Hence, as previously reported in [4], the presence or absence of coherent, current/pressure-driven (low-frequency) and higher frequency fast-ion driven modes can be discounted to explain the anomalous ion heating observed with the αs.…”
Section: Measurements Of the Ion And Electron Drift-wave Turbulence Smentioning
confidence: 78%
“…Hence, knowledge of the noise level in the measurements helps one to determine the optimum value for λ NORM to be used for the analysis of the turbulence data. As an example of this efficient tuning of λ NORM , this quantity is set in the range λ NORM = 0.10 to λ NORM = 0.35 when performing the analysis of the very long time series typical of astronomical and astrophysical measurements [7], then λ NORM = 0.85 to λ NORM = 0.95 when performing in real-time the toroidal mode number decomposition of the frequencydegenerate spectrum of coherent AEs actively driven by an in-vessel antenna system in JET [52,72], so that only the largest component is selected for real-time tracking [73,74], then λ NORM = 0.35 to λ NORM = 0.95 when the same analysis is performed post-pulse, so that effectively all (or a selection of the largest between) the coherent, antenna-driven AEs whose amplitude is well above the background turbulence level are…”
Section: Appendix a The Sparse Representation Methods And The Sparspementioning
confidence: 99%
“…This expression allows an exact and quick calculation of the excitation n-spectrum without the need to repeat the Fourier calculation for different values of the antenna currents. By fitting the measured transfer function H = H(n, ω) to a rational function as described in [19], one obtains the frequency and damping rate of individual modes. Such a fit is shown for 2 modes of n = ±5 in figure 7.…”
Section: Damping Rate Measurements Of N = 3 − 5 Taesmentioning
confidence: 99%
“…is constructed from the input data, as described in [19]. The input data are synchronously detected signals.…”
Section: Real-time N-decomposition Of the Plasma Response Using Sparspecmentioning
confidence: 99%
“…By exciting modes with external antennas in Ohmic plasmas with no fast particle drive, it is possible to isolate the damping from the drive mechanisms. Previous work on JET [7][8][9][10][11] has extensively studied the damping rates of low n = 0, 1, and 2 stable AEs excited with large saddle coils across a broad range of plasma conditions, where they have found a clear dependence of the damping, for example, on plasma shape and edge magnetic shear. The damping rate was found to increase with increased triangularity and elongation consistent with the increased edge magnetic shear.…”
Section: Introductionmentioning
confidence: 99%