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Evidence of “Two Plasmon” Decay of Energetic Particle Induced Geodesic Acoustic Mode

Zhiyong Qiu1,2, Liu Chen1,2,3, Fulvio Zonca2,1 and Matteo Valerio Falessi2 1Institute for Fusion Theory and Simulation and Department of Physics, Zhejiang University, Hangzhou, P.R.C 2 Center for Nonlinear Plasma Science and ENEA C. R. Frascati, Frascati, Italy 3Department of Physics and Astronomy, University of California, Irvine CA 92697-4575, U.S.A.
Abstract

Secondary low frequency mode generation by energetic particle induced geodesic acoustic mode (EGAM) observed in LHD experiment is studied using nonlinear gyrokinetic theory. It is found that the EGAM frequency can be significantly higher than local geodesic acoustic mode (GAM) frequency in low collisionality plasmas, and it can decay into two GAMs as its frequency approaches twice GAM frequency, in a process analogous to the well-known two plasmon decay instability. The condition for this process to occur is also discussed.

1 Introduction

Confinement of plasmas in magnetically confined fusion devices [1] is one of the key issues for the sustained burning and fusion gain. The anomalous transport induced by micro-scale turbulence excited by expansion free energy intrinsic to confinement is thus an important topic of fusion plasma research [2, 3]. Zonal field structures (ZFS) with toroidally and nearly poloidally symmetric mode structures (n=0/m0,±1n=0/m\simeq 0,\pm 1\cdots, with n/mn/m being the toroidal/poloidal mode numbers, respectively) are generally recognized to regulate micro-scale drift wave turbulence (DW) including drift Alfvén waves (DAWs) and their associated transport by scattering into stable short radial wavelength regimes [4, 5, 6, 7, 8]. Interested readers may refer to a recent work [9] discussing the role of ZFS and phase space zonal structures (PSZS) [10, 11] as the generator of nonlinear equilibria with (suppressed) turbulence [6, 12].

Geodesic acoustic modes (GAMs) [13, 14] are ZFS unique in toroidal plasmas; oscillating at a finite frequency in the ion sound frequency regime due to toroidicity induced plasma compression. GAMs are predominantly electrostatic radial corrugations with the scalar potential characterized by n=0/m0,±1,n=0/m\simeq 0,\pm 1,\cdots, and an up-down anti-symmetric m1m\simeq 1 density perturbation. Consequently, GAM, being toroidally symmetric, cannot by itself induce cross-field transport. Instead, GAMs can regulate DW/DAWs and the associated transport via spontaneous excitation, since they can scatter DW/DAWs into stable short radial wavelength domain [15, 14, 16, 17]. Interested readers may refer to Ref. [18] for a brief review of kinetic theories of GAM, including linear dispersion relation, excitation by super-thermal energetic particles (EPs) and nonlinear interaction with DWs/DAWs.

Due to their finite frequencies, GAMs can resonantly interact and exchange energy with charged particles including super-thermal EPs, leading to, respectively, collisionless Landau damping [19, 20] and resonant excitation by EPs [21, 22, 23]. The excitation of EP-induced GAM (EGAM) was first analytically investigated in Ref. [24], showing the dominant role played by wave-particle resonant interactions and free energy associated with EP velocity space anisotropy, with application to different scenarios characterized by different EP distribution functions [25, 26, 27, 28, 29, 30]. The global features due to GAM continuum coupling are also investigated [31], yielding a finite threshold due to continuum damping, or mode conversion to propagating kinetic GAM, as kinetic dispersiveness of both thermal and energetic ions are properly accounted for [26, 32]. The EGAMs are typically characterized by a global mode structure with frequency lower than local GAM frequency and radial extension determined by EP density profile and kinetic dispersiveness, LLnρhL\sim\sqrt{L_{n}\rho_{h}}, with LnL_{n} being the EP density profile scale length, and ρh\rho_{h} being EP characteristic orbit width. Nonlinear saturation of EGAM due to wave-particle trapping [33] in the weak drive limit is investigated [34, 35], and the EGAM induced EP loss via pitch angle scattering into unconfined orbits is presented in Ref. [36].

Recently, a peculiar phenomena was reported in Large Helical Device (LHD) low density experiments with neutral beam injection (NBI) heating [23]. During the discharge with relatively high plasma temperature (central electron temperature up to \sim 7keV) and low plasma density (line averaged density 0.1×1019m3\sim 0.1\times 10^{19}m^{-3}), the EGAM frequency is observed to be significantly higher than local GAM frequency. The interpretation was given in Ref. [30], where it was shown that, due to the low collisionality in the high-temperature/low-density discharges, the injected beam ions are not fully slowed down, and form a bump-on-tail type EP distribution function. As a consequence, the free energy associated with the positive slope in the low energy side of the distribution function, provides an additional drive, that generates a new unstable branch with the frequency being significantly higher than local GAM frequency [30]. A similar interpretation was also provided in Ref. [29] considering a similar distribution function induced by low charge exchange rate.

It was further found [37] that, as the high frequency EGAM (will be denoted as “primary EGAM” in the rest of the paper for apparent reasons) chirped up to twice local GAM frequency, possibly as a result of the EGAM induced pitch angle scattering to lower pitch angle and thus higher vv_{\parallel} domain, a “secondary mode” could be strongly driven unstable, with the frequency close to the local GAM frequency [37]. The experimental observations are nicely recovered in a MHD-kinetic hybrid simulation using MEGA code [38, 39], and it is found that, besides the secondary mode strong excitation, the EPs “driving” the secondary mode are the same as those linearly driving the primary EGAM, though the secondary mode frequency is only half of that of the primary mode. It is also found that the secondary mode generation still persists when the “fluid nonlinearity” is turned off; and, as the primary mode frequency keeps chirping up, the secondary mode frequency is almost unchanged, suggesting it is a normal mode of the system itself. One speculation by Ref. [39] is that the secondary mode is driven by “nonlinear resonance” [40, 41], which, however, is typically associated with finite amplitude fluctuations, and is not satisfied in the condition for the onset of the secondary mode.

In this work, we will show that, the mechanism underlying the secondary mode generation observed in Ref. [37] is analogous to the well-known two plasmon decay process [42, 43], where an incident electromagnetic wave decays into two plasma waves identical to each other. The primary mode corresponds to the linearly unstable high frequency EGAM given in Ref. [30], while the secondary mode corresponds to a linearly stable branch described by the same linear dispersion relation, with the frequency determined by the local GAM frequency. The secondary mode can be nonlinearly driven unstable as the primary mode frequency approaches twice the secondary mode frequency (which is close to the local GAM frequency), which minimizes the threshold due to frequency mismatch. The interpretation is consistent with the crucial elements from experimental observation [37] and numerical simulation [39]; thus, it provides and illuminates the underlying physics picture.

The rest of the paper is organized as follows. In Sec. 2, the theoretical model is given. The linear particle response to EGAM is derived in Sec. 3, where the linear EGAM properties in the LHD low collisionality plasma are also reviewed. In Sec. 4, the nonlinear decay of the primary mode into two low frequency GAMs is investigated, and its correspondence to the experimental observations and MEGA simulations are discussed. Finally, a brief summary and discussion is presented in Sec. 5. For the self-containedness of the materials, the properties of the three branches of the linear dispersion relation are briefly reproduced in A, while the frequency up-chirping of the primary EGAM, being an important condition for the decay process, is briefly outlined in B.

2 Theoretical Model

In the above described nonlinear decay process, a primary EGAM (Ω0Ω0(ω0,kr,0)\Omega_{0}\equiv\Omega_{0}(\omega_{0},k_{r,0})) decays into two secondary modes with almost identical frequency, Ω1Ω1(ω1,kr,1)\Omega_{1}\equiv\Omega_{1}(\omega_{1},k_{r,1}) and Ω2Ω2(ω2,kr,2)\Omega_{2}\equiv\Omega_{2}(\omega_{2},k_{r,2}). All the three modes, are EGAM/GAMs with n=0/m0n=0/m\simeq 0, thus the toroidal/poloidal wavenumber matching condition is naturally satisfied, and only the constraint on frequency and radial wavenumber matching condition is needed. For the modes with predominantly electrostatic polarization, the equations describing the nonlinear decay of the linearly unstable primary EGAM, can be derived from the charge quasi-neutrality condition. Assuming for simplicity the bulk ions and EPs are the same ion species with unit electric charge, the quasi-neutrality condition can be written as:

δne=δni+δnh,\displaystyle\delta n_{e}=\delta n_{i}+\delta n_{h}, (1)

with the perturbed particle density derived from the perturbed distribution function as

δns(q/m)EF0,sδϕ+J0(kρL,s)δHs.\displaystyle\delta n_{s}\equiv\left\langle(q/m)\partial_{E}F_{0,s}\delta\phi+J_{0}(k_{\perp}\rho_{L,s})\delta H_{s}\right\rangle. (2)

Here, subscripts s=e,i,hs=e,i,h denote electrons, ions and energetic (hot) particles, respectively, F0,sF_{0,s} is the equilibrium distribution function, EF0,s\partial_{E}F_{0,s} is the short notation for F0,s/E\partial F_{0,s}/\partial E, with Ev2/2E\equiv v^{2}/2, J0(kρL,s)J_{0}(k_{\perp}\rho_{L,s}) is the Bessel function of zero index accounting for finite Larmor radius (FLR) effects, kk_{\perp} is the perpendicular wavenumber, ρLv/Ωs\rho_{L}\equiv v_{\perp}/\Omega_{s} is the Larmor radius with Ωs\Omega_{s} being gyro-frequency, and \langle\cdots\rangle denotes velocity space integration. δH\delta H is the non-adiabatic particle response to GAM/EGAM, and can be derived from nonlinear gyrokinetic equation [44]:

(t+ωtrθ+iωd)δHk\displaystyle\left(\partial_{t}+\omega_{tr}\partial_{\theta}+i\omega_{d}\right)\delta H_{k} =\displaystyle= iωqmEF0Jkδϕk\displaystyle-i\omega\frac{q}{m}\partial_{E}F_{0}J_{k}\delta\phi_{k} (3)
cB0𝐤=𝐤+𝐤′′𝐛^𝐤′′×𝐤JkδϕkδHk′′.\displaystyle-\frac{c}{B_{0}}\sum_{\mathbf{k}=\mathbf{k^{\prime}}+\mathbf{k^{\prime\prime}}}\hat{\mathbf{b}}\cdot\mathbf{k}^{\prime\prime}\times\mathbf{k}^{\prime}J_{k^{\prime}}\delta\phi_{k^{\prime}}\delta H_{k^{\prime\prime}}.

Here, ωtrv/(qR0)\omega_{tr}\equiv v_{\parallel}/(qR_{0}) is the transit frequency, ωd=krvd\omega_{d}=k_{r}v_{d} is the magnetic drift frequency associated with geodesic curvature, and vd=(v2+2v2)sinθ/(2ΩR0)v^dsinθv_{d}=(v^{2}_{\perp}+2v^{2}_{\parallel})\sin\theta/(2\Omega R_{0})\equiv\hat{v}_{d}\sin\theta is the magnetic drift velocity, JkJ0(kρL)J_{k}\equiv J_{0}(k_{\perp}\rho_{L}) for simplicity of notation, and 𝐤=𝐤+𝐤′′\sum_{\mathbf{k}=\mathbf{k^{\prime}}+\mathbf{k^{\prime\prime}}} denotes the usual selection rule for frequency/wavenumber matching condition for the nonlinear mode coupling. The other notations are standard.

The thermal plasma linear response to GAM/EGAM, can be readily obtained from Ref. [20], and after surface averaging, equation (1) reduces to

emin0kr21Ωi2(1ωG2ω2)δϕ¯k+δn¯iNL+δn¯h=0,\displaystyle-\frac{e}{m_{i}}n_{0}k^{2}_{r}\frac{1}{\Omega^{2}_{i}}\left(1-\frac{\omega^{2}_{G}}{\omega^{2}}\right)\overline{\delta\phi}_{k}+\overline{\delta n}^{NL}_{i}+\overline{\delta n}_{h}=0, (4)

with the leading order linear thermal plasma response properly accounted for by the first term, from which the linear dispersion relation of GAM can be obtained, and ()¯02π()𝑑θ/(2π)\overline{(\cdots)}\equiv\int^{2\pi}_{0}(\cdots)d\theta/(2\pi) is the surface averaging. Furthermore, ωG7/4+τvit/R\omega_{G}\equiv\sqrt{7/4+\tau}v_{it}/R is the leading order GAM frequency with τ=Te/Ti\tau=T_{e}/T_{i} being the temperature ratio and vitv_{it} being ion thermal velocity, while higher order terms such as FLR and/or finite parallel compression can be straightforwardly accounted for by replacing ωG\omega_{G} with more accurate expression [20]. The linear EGAM dispersion relation can be derived by keeping δnhL\delta n^{L}_{h} in equation (4), with the free energy from EP velocity space anisotropy and the characteristic features of the EGAM determined by the specific EP distribution function [24, 25, 26, 30, 29]. Nonlinear modulation of GAM/EGAM by thermal plasma nonlinearity, can be accounted for by δniNL\delta n^{NL}_{i}, including excitation by DW/DAWs [14, 45, 16]. Here, super-scripts “L” and “NL” represent linear and nonlinear responses, respectively.

For the LHD low collisionality discharge [23] of interest, where plasma density is very low while the electron temperature is very high, the EP is characterized by a not fully slowed down distribution function, analogous to a bump-on-tail case, and the corresponding linear properties of the EGAM are investigated in Ref. [30]. The linear EGAM properties are the basis of the present nonlinear analysis, and, thus, for the self-containedness of the present nonlinear analysis, the results of Ref. [30] will be briefly summarized in Sec. 3

In this work, both the thermal plasma and EP induced nonlinear coupling are consistently derived [46, 47], by including their nonlinear contribution to density perturbation in the quasi-neutrality condition. As we will show a posteriori, the nonlinear coupling is dominated by the EP finite orbit width effects (FoWs), with resonant EPs playing the crucial role [48, 47]. The thermal plasma contribution to the nonlinear coupling [46], meanwhile, will be shown to be negligible compared to the dominant role of EPs.

3 Linear properties

For the completeness of this work, we will briefly derive the linear EP response to GAM/EGAM, which will be used in deriving the nonlinear response of EP to the secondary EGAMs. Separating the linear from nonlinear responses by taking δHk=δHkL+δHkNL\delta H_{k}=\delta H^{L}_{k}+\delta H^{NL}_{k}, the linear EP response to EGAM can be derived from the linear gyrokinetic equation,

(t+ωtrθ+iωd)δHkL=iωemEF0Jkδϕk.\displaystyle\left(\partial_{t}+\omega_{tr}\partial_{\theta}+i\omega_{d}\right)\delta H^{L}_{k}=-i\omega\frac{e}{m}\partial_{E}F_{0}J_{k}\delta\phi_{k}. (5)

Equation (5) can be solved by transforming into the EP drift orbit center coordinate by taking δHkLeiΛkδHdkL\delta H^{L}_{k}\equiv e^{i\Lambda_{k}}\delta H^{L}_{dk}, with Λk\Lambda_{k} satisfying ωtrθΛk+ωd,k=0\omega_{tr}\partial_{\theta}\Lambda_{k}+\omega_{d,k}=0. Here, for simplicity of discussion and focus on proof of principle demonstration, well circulating EPs are assumed, thus, variation of vv_{\parallel} along the magnetic field is neglected, and one has Λk=Λ^kcosθ\Lambda_{k}=\hat{\Lambda}_{k}\cos\theta, with Λ^k=krρ^d\hat{\Lambda}_{k}=k_{r}\hat{\rho}_{d} being radial wave-number normalized to drift orbit width, and ρ^d=v^dr/ωtr\hat{\rho}_{d}=\hat{v}_{dr}/\omega_{tr} is the EP magnetic drift orbit width. The generalization to finite inverse aspect ratio case as well as general geometry and particle orbits is straightforward. Furthermore, τTe/Ti1\tau\equiv T_{e}/T_{i}\ll 1 is assumed for simplicity, such that one has δϕGδϕ¯G\delta\phi_{G}\simeq\overline{\delta\phi}_{G} while ωtr,eωG\omega_{tr,e}\gg\omega_{G} is still satisfied 111Interested readers may refer to Ref. [20] for the contribution of finite τ\tau to linear GAM dispersion relation via the m0m\neq 0 components of the scalar potential.. We then have,

(t+ωtrθ)δHdkL=emeiΛ^kcosθJktδϕ¯kEF0,h,\displaystyle\left(\partial_{t}+\omega_{tr}\partial_{\theta}\right)\delta H^{L}_{dk}=-\frac{e}{m}e^{-i\hat{\Lambda}_{k}\cos\theta}J_{k}\partial_{t}\overline{\delta\phi}_{k}\partial_{E}F_{0,h}, (6)

from which δHdkL\delta H^{L}_{dk} can be derived as

δHdkL=emEF0,hJkδϕ¯kl=ωωlωtr(i)lJl(Λ^k)eilθ.\displaystyle\delta H^{L}_{dk}=-\frac{e}{m}\partial_{E}F_{0,h}J_{k}\overline{\delta\phi}_{k}\sum^{\infty}_{l=-\infty}\frac{\omega}{\omega-l\omega_{tr}}(-i)^{l}J_{l}(\hat{\Lambda}_{k})e^{il\theta}. (7)

Here, ll is integer, and ll=\sum_{l}\equiv\sum_{l=-\infty}^{\infty} will be used later for simplicity of notation. In deriving equation (7), the Jacobi-Anger expansion eiΛ^kcosθ=lilJl(Λ^k)eilθe^{i\hat{\Lambda}_{k}\cos\theta}=\sum_{l}i^{l}J_{l}(\hat{\Lambda}_{k})e^{il\theta} is used. Pulling back to the EP guiding center coordinate, we then have, the linear well-circulating EP response to EGAM

δHkL=emEF0,hJkδϕ¯kl,pωωlωtril+pJl(Λ^k)Jp(Λ^k)ei(l+p)θ.\displaystyle\delta H^{L}_{k}=-\frac{e}{m}\partial_{E}F_{0,h}J_{k}\overline{\delta\phi}_{k}\sum_{l,p}\frac{\omega}{\omega-l\omega_{tr}}i^{-l+p}J_{l}(\hat{\Lambda}_{k})J_{p}(\hat{\Lambda}_{k})e^{i(l+p)\theta}. (8)

Substituting equation (8) into the surface averaged quasi-neutrality condition, equation (4), one then obtains,

emin0kr21Ωi2EGAMδϕ¯=0,\displaystyle\frac{e}{m_{i}}n_{0}k^{2}_{r}\frac{1}{\Omega^{2}_{i}}\mathscr{E}_{EGAM}\overline{\delta\phi}=0, (9)

with the EGAM dispersion relation given by

EGAM\displaystyle\mathscr{E}_{EGAM}\equiv 1+ωG2ω2\displaystyle-1+\frac{\omega^{2}_{G}}{\omega^{2}} (10)
+2πB0e2n0(2λB0)2(1λB0)1/2E5/2dEdλEF0,h2E(1λB0)ω2q2R02.\displaystyle+\frac{\sqrt{2}\pi B_{0}e^{2}}{n_{0}}\int\frac{(2-\lambda B_{0})^{2}}{(1-\lambda B_{0})^{1/2}}\frac{E^{5/2}dEd\lambda\partial_{E}F_{0,h}}{2E(1-\lambda B_{0})-\omega^{2}q^{2}R^{2}_{0}}.

Here, only the l=±1l=\pm 1 transit harmonic are kept in equation (10), in consistency with the typical Λ^k1\hat{\Lambda}_{k}\ll 1 ordering for EGAMs with global mode structure. The EGAM stability depends sensitively on the specific EP equilibrium distribution function. For the not fully slowed down EPs in LHD experiments [23] due to low collisionality, the distribution can be modelled as

F0,h=c0H(EbE)H(EEL)E3/2+Ecrit3/2δ(λλ0),\displaystyle F_{0,h}=\frac{c_{0}H(E_{b}-E)H(E-E_{L})}{E^{3/2}+E^{3/2}_{crit}}\delta(\lambda-\lambda_{0}), (11)

which can be solved as a dynamic solution of the Fokker-Planck equation with the collisional operator dominated by thermal electron induced slowing down [30]. Here, λμB0/E\lambda\equiv\mu B_{0}/E is the pitch angle, μmv2/B\mu\equiv mv^{2}_{\perp}/B is the magnetic moment, H(λλ0)H(\lambda-\lambda_{0}) is the Heaviside step function, EbE_{b} is the EP birth energy, ELEbexp(2γct)E_{L}\simeq E_{b}\exp(-2\gamma_{c}t) is the time dependent lower end of the distribution function, and EcritE_{crit} is the critical energy at which the EP pitch angle scattering rate off thermal ions is comparable with the slowing down rate γc\gamma_{c} [49]. The normalization to EP density nbn_{b} gives c0=nb1λ0B0/(22πB0ln(Eb/EL))c_{0}=n_{b}\sqrt{1-\lambda_{0}B_{0}}/(2\sqrt{2}\pi B_{0}\ln(E_{b}/E_{L})). Note that, c0c_{0} is proportional to Γ/γc\Gamma/\gamma_{c} with Γ\Gamma being the NBI particle flux and γc\gamma_{c} is the slowing-down rate on thermal electrons. The resulting dispersion relation is given as [30]

1+ωG2ω2+Nb[C(ln(1ωb2ω2)ln(1ωL2ω2))\displaystyle-1+\frac{\omega^{2}_{G}}{\omega^{2}}+N_{b}\left[C\left(\ln\left(1-\frac{\omega^{2}_{b}}{\omega^{2}}\right)-\ln\left(1-\frac{\omega^{2}_{L}}{\omega^{2}}\right)\right)\right.
+D(11ωb2/ω211ωL2/ω2)]=0.\displaystyle\left.+D\left(\frac{1}{1-\omega^{2}_{b}/\omega^{2}}-\frac{1}{1-\omega^{2}_{L}/\omega^{2}}\right)\right]=0. (12)

Here, Nbnbq21λ0B0/(4ln(Eb/EL)n0)N_{b}\equiv n_{b}q^{2}\sqrt{1-\lambda_{0}B_{0}}/(4\ln(E_{b}/E_{L})n_{0}) is the ratio of EP to bulk plasma density, C=(2λ0B0)(5λ0B02)/(2(1λ0B0)5/2)C=(2-\lambda_{0}B_{0})(5\lambda_{0}B_{0}-2)/(2(1-\lambda_{0}B_{0})^{5/2}), D=λ0B0(2λ0B0)2/(1λ0B0)5/2D=\lambda_{0}B_{0}(2-\lambda_{0}B_{0})^{2}/(1-\lambda_{0}B_{0})^{5/2}, and ωb2Eb(1λ0B0)/(qR0)\omega_{b}\equiv\sqrt{2E_{b}(1-\lambda_{0}B_{0})}/(qR_{0}) and ωL2EL(1λ0B0)/(qR0)\omega_{L}\equiv\sqrt{2E_{L}(1-\lambda_{0}B_{0})}/(qR_{0}) are the transit frequencies defined at EbE_{b} and ELE_{L}, respectively. The first term in the square bracket corresponds to the slowing-down distribution induced logarithmic singularity, and it is destabilizing for λ0B0>2/5\lambda_{0}B_{0}>2/5 [26]; while the single pole like singularity in the second term is from the low energy side cutoff, and it is always destabilizing [30].

The dispersion relation (12) have three branches, i.e., an unstable branch determined by and close to ωL\omega_{L}, and is denoted as “lower beam branch” (LBB); a stable branch determined by the local GAM frequency, denoted as the “GAM branch” (GB), and is little affected by the EP distribution function; and a marginally stable branch determined by the birth energy of the distribution function (EbE_{b}), and is denoted as “upper beam branch” (UBB). It is noteworthy that, the unstable LBB can have a frequency much higher than the local GAM frequency, while γ/ωGNb\gamma/\omega_{G}\propto\sqrt{N_{b}} can be obtained by balancing the thermal plasma contribution to the dominant destabilizing term due to low energy end cutoff (i.e., the term proportional to 1/(1ωL2/ω2)1/(1-\omega^{2}_{L}/\omega^{2}) in equation (12)). The stability of the three branches described by the dispersion relation (12) on ωL\omega_{L} is briefly summarized in A for the convenience of readers. One important feature is that, the linear unstable LBB frequency is non-perturbatively determined by ωL\omega_{L}, and thus, will self-consistently chirp up or down, due to EGAM induced pitch angle scattering, as we show in B.

Thus, the primary mode in LHD experiment [23] corresponds to the linearly unstable LBB, while the secondary mode with the frequency being local GAM frequency, corresponds to the linearly stable GB. We will show in the next section that, as the unstable LBB chirping up to twice local GAM frequency, it can decay into two linearly stable GBs, similar to the well-known “two plasmon decay” process describing an electromagnetic wave decay into two Langmuir waves [42, 43].

4 Two plasmon decay of EGAM

In this section, the high frequency LBB decay into two linearly stable GBs, will be investigated using nonlinear gyrokinetic theory. Denoting the “primary mode” and two “secondary modes” with subscripts “0”, “1” and “2”, respectively, the nonlinear particle responses to GAM/EGAM can be derived from nonlinear gyrokinetic equation

(t+ωtrθ+iωd)δHkNL=cB0𝐤=𝐤′′+𝐤𝐛^𝐤′′×𝐤Jkδϕ¯kδHk′′.\displaystyle\left(\partial_{t}+\omega_{tr}\partial_{\theta}+i\omega_{d}\right)\delta H^{NL}_{k}=-\frac{c}{B_{0}}\sum_{\mathbf{k}=\mathbf{k}^{\prime\prime}+\mathbf{k}^{\prime}}\hat{\mathbf{b}}\cdot\mathbf{k}^{\prime\prime}\times\mathbf{k^{\prime}}J_{k^{\prime}}\overline{\delta\phi}_{k^{\prime}}\delta H_{k^{\prime\prime}}. (13)

To properly assess the nonlinear coupling, the contribution of both thermal plasmas and EPs are considered simultaneously, by deriving their nonlinear response to GAM/EGAM, and evaluating their contribution to the surface averaged quasi-neutrality condition, equation (4).

4.1 Negligible thermal plasma contribution to nonlinear coupling

For electrons with ωtr,eωG\omega_{tr,e}\gg\omega_{G}, the nonlinear electron response is dominated by surface averaged contribution. Noting δHeL=(e/Te)F0,eδϕ¯k\delta H^{L}_{e}=(e/T_{e})F_{0,e}\overline{\delta\phi}_{k}, one has

tδHk,eNL=cB0k𝐛^𝐤′′×𝐤δϕ¯keTeF0,eδϕ¯k′′=0,\displaystyle\partial_{t}\delta H^{NL}_{k,e}=-\frac{c}{B_{0}}\sum_{k}\hat{\mathbf{b}}\cdot\mathbf{k^{\prime\prime}}\times\mathbf{k^{\prime}}\overline{\delta\phi}_{k^{\prime}}\frac{e}{T_{e}}F_{0,e}\overline{\delta\phi}_{k^{\prime\prime}}=0, (14)

i.e., δHk,eNL=0\delta H^{NL}_{k,e}=0 up to the O(ωG/ωtr,e)1O(\omega_{G}/\omega_{tr,e})\ll 1 order. Thus, electron contribution to the nonlinear coupling can be neglected.

Nonlinear ion response can be derived, noting the ωGωtr,i,ωd\omega_{G}\gg\omega_{tr,i},\omega_{d} ordering and that δHiL(e/Ti)J0δϕ¯G(1+ωd/ω)\delta H^{L}_{i}\simeq-(e/T_{i})J_{0}\overline{\delta\phi}_{G}(1+\omega_{d}/\omega), and one has

tδHk,iNL\displaystyle\partial_{t}\delta H^{NL}_{k,i} \displaystyle\simeq cB0k𝐛^𝐤′′×𝐤Jkδϕ¯kδHk′′\displaystyle-\frac{c}{B_{0}}\sum_{k}\hat{\mathbf{b}}\cdot\mathbf{k^{\prime\prime}}\times\mathbf{k^{\prime}}J_{k^{\prime}}\overline{\delta\phi}_{k^{\prime}}\delta H_{k^{\prime\prime}} (15)
\displaystyle\simeq cB0[Jkrδϕ¯k1rθδHi,k′′LJk′′rδϕ¯k′′1rθδHi,kL].\displaystyle-\frac{c}{B_{0}}\left[J_{k^{\prime}}\partial_{r}\overline{\delta\phi}_{k^{\prime}}\frac{1}{r}\partial_{\theta}\delta H^{L}_{i,k^{\prime\prime}}-J_{k^{\prime\prime}}\partial_{r}\overline{\delta\phi}_{k^{\prime\prime}}\frac{1}{r}\partial_{\theta}\delta H^{L}_{i,k^{\prime}}\right].

Note that, for GAM/EAM with n=0n=0, the geodesic curvature induced drift ωdsinθ\omega_{d}\propto\sin\theta, which gives δHk,iNL\delta H^{NL}_{k,i} a cosθ\propto\cos\theta dependence to the leading order. Thus, finite contribution to the surface averaged quasi-neutrality can only enter through toroidal coupling (B1ϵcosθB\propto 1-\epsilon\cos\theta), as was discussed in Ref. [50]. Thus, the thermal ion induced nonlinearity via surfaced averaged quasi-neutrality condition, can be estimated to be of order cϵn0krδϕ0δϕ1ωd,i/(ωGrB0)\sim c\epsilon n_{0}k_{r}\delta\phi_{0}\delta\phi_{1}\omega_{d,i}/(\omega_{G}rB_{0}), which is comparable to parallel nonlinearity and is, thus, negligibly small. Consequently, we expect the EP induced nonlinear coupling will be dominant, as shown in Refs. [48, 47].

4.2 Finite EP contribution to nonlinear coupling via EP FoW effects

Nonlinear EP response to the sideband Ωk\Omega_{k} can be derived from nonlinear gyrokinetic equation, by drift orbit center coordinate transformation. For the Ω1\Omega_{1} generation due to the coupling of Ω0\Omega_{0} and Ω2\Omega_{2^{*}} coupling, taking δH1NL=eiΛ1δHd1NL\delta H^{NL}_{1}=e^{i\Lambda_{1}}\delta H^{NL}_{d1}, the corresponding equation for nonlinear EP response to Ω1\Omega_{1} can be written as

(t+ωtrθ)δHd1NL\displaystyle\left(\partial_{t}+\omega_{tr}\partial_{\theta}\right)\delta H^{NL}_{d1} =cB0eiΛ1𝐤1𝐛^𝐤′′×𝐤Jkδϕ¯kδHh,k′′L\displaystyle=-\frac{c}{B_{0}}e^{-i\Lambda_{1}}\sum_{\mathbf{k}_{1}}\hat{\mathbf{b}}\cdot\mathbf{k^{\prime\prime}}\times\mathbf{k^{\prime}}J_{k^{\prime}}\overline{\delta\phi}_{k^{\prime}}\delta H^{L}_{h,k^{\prime\prime}} (16)
=crB0eiΛ1[rδϕ¯2θδH0Lrδϕ¯0θδH2L].\displaystyle=-\frac{c}{rB_{0}}e^{-i\Lambda_{1}}\left[\partial_{r}\overline{\delta\phi}_{2^{*}}\partial_{\theta}\delta H^{L}_{0}-\partial_{r}\overline{\delta\phi}_{0}\partial_{\theta}\delta H^{L}_{2^{*}}\right].

Here, one expects that the contribution from δϕ¯2δH0L\overline{\delta\phi}_{2^{*}}\delta H^{L}_{0} being dominant with respect to δϕ¯0δH2L\overline{\delta\phi}_{0}\delta H^{L}_{2^{*}} due to the crucial contribution of resonant EPs (note that Ω0\Omega_{0} is linearly unstable due to resonant EP drive). However, both terms are consistently kept for now, with both resonant and non-resonant EP contribution to the nonlinear coupling accounted for on the same footing. As we will show a posteriori, the nonlinear coupling is dominated by EP FoW effects, while the sub-dominant EP FLR effects can be neglected systematically. Substituting the linear EP response into equation (16), we then have,

δHd,1NL\displaystyle\delta H^{NL}_{d,1} =\displaystyle= crB0emEF0,hl,p,ηJη(Λ^1)iηeiηθ\displaystyle-\frac{c}{rB_{0}}\frac{e}{m}\partial_{E}F_{0,h}\sum_{l,p,\eta}J_{\eta}(\hat{\Lambda}_{1})i^{-\eta}e^{i\eta\theta}
×\displaystyle\times [rδϕ¯2δϕ¯0i(l+p)ω0ω0lωtrJl(Λ^0)Jp(Λ^0)ω1(l+p+η)ωtril+pei(l+p)θ\displaystyle\left[\partial_{r}\overline{\delta\phi}_{2^{*}}\overline{\delta\phi}_{0}\frac{i(l+p)\omega_{0}}{\omega_{0}-l\omega_{tr}}\frac{J_{l}(\hat{\Lambda}_{0})J_{p}(\hat{\Lambda}_{0})}{\omega_{1}-(l+p+\eta)\omega_{tr}}i^{-l+p}e^{i(l+p)\theta}\right.
\displaystyle- rδϕ¯0δϕ¯2i(l+p)ω2ω2lωtrJl(Λ^2)Jp(Λ^2)ω1(l+p+η)ωtrilpei(l+p)θ].\displaystyle\left.\partial_{r}\overline{\delta\phi}_{0}\overline{\delta\phi}_{2^{*}}\frac{i(l+p)\omega_{2^{*}}}{\omega_{2^{*}}-l\omega_{tr}}\frac{J_{l}(\hat{\Lambda}_{2})J_{p}(\hat{\Lambda}_{2})}{\omega_{1}-(-l+p+\eta)\omega_{tr}}i^{l-p}e^{i(-l+p)\theta}\right].

The nonlinear EP response to Ω1\Omega_{1} can then be obtained, by the pull-back transformation, and one has

δH1NL\displaystyle\delta H^{NL}_{1} =\displaystyle= icrB0emEF0,hl,p,η,hJη(Λ^1)Jh(Λ^1)iη+hei(η+h)θ\displaystyle-i\frac{c}{rB_{0}}\frac{e}{m}\partial_{E}F_{0,h}\sum_{l,p,\eta,h}J_{\eta}(\hat{\Lambda}_{1})J_{h}(\hat{\Lambda}_{1})i^{-\eta+h}e^{i(\eta+h)\theta} (17)
×\displaystyle\times [rδϕ¯2δϕ¯0(l+p)ω0ω0lωtrJl(Λ^0)Jp(Λ^0)ω1(l+p+η)ωtril+pei(l+p)θ\displaystyle\left[\partial_{r}\overline{\delta\phi}_{2^{*}}\overline{\delta\phi}_{0}\frac{(l+p)\omega_{0}}{\omega_{0}-l\omega_{tr}}\frac{J_{l}(\hat{\Lambda}_{0})J_{p}(\hat{\Lambda}_{0})}{\omega_{1}-(l+p+\eta)\omega_{tr}}i^{-l+p}e^{i(l+p)\theta}\right.
\displaystyle- rδϕ¯0δϕ¯2(l+p)ω2ω2lωtrJl(Λ^2)Jp(Λ^2)ω1(l+p+η)ωtrilpei(l+p)θ].\displaystyle\left.\partial_{r}\overline{\delta\phi}_{0}\overline{\delta\phi}_{2^{*}}\frac{(l+p)\omega_{2^{*}}}{\omega_{2^{*}}-l\omega_{tr}}\frac{J_{l}(\hat{\Lambda}_{2})J_{p}(\hat{\Lambda}_{2})}{\omega_{1}-(-l+p+\eta)\omega_{tr}}i^{l-p}e^{i(-l+p)\theta}\right].

In the above expression, the first term in the bracket comes from δϕ¯2δH0L\overline{\delta\phi}_{2^{*}}\delta H^{L}_{0}, as evident from the denominator ω0lωtr\omega_{0}-l\omega_{tr}, while the other term comes from δϕ¯0δH2L\overline{\delta\phi}_{0}\delta H^{L}_{2^{*}}. For simplicity, in the following derivation, only the first term due to δϕ¯2δH0L\overline{\delta\phi}_{2^{*}}\delta H^{L}_{0} will be kept, which can be dominant due to resonant EP contribution. The other term, can also contribute and quantitatively impact the nonlinear process, but we expect its contribution is relatively small. The physics meaning of various terms in equation (17) is clear, in that ω0lωtr\omega_{0}-l\omega_{tr} in the denominator gives wave-particle power exchanges with the pump Ω0\Omega_{0}, (l+p)(l+p) comes from θδH0L\partial_{\theta}\delta H^{L}_{0} in the perpendicular nonlinearity, and the Bessel functions are from EP FoW effects, determining the strength of EPs interaction with the mode.

For finite Ω1\Omega_{1} generation due to δH1NL¯\overline{\langle\delta H^{NL}_{1}\rangle}, assuming |Λ^k|1|\hat{\Lambda}_{k}|\ll 1 for EGAMs with typically global mode structure, one requires the following “selection rules” for non-vanishing EP contribution: 1. l+p+η+h=0l+p+\eta+h=0 for non-vanishing component surface average, 2. l+p0l+p\neq 0 for θδH0L0\partial_{\theta}\delta H^{L}_{0}\neq 0, 3. l0l\neq 0 for finite EP linear drive to the primary EGAM, and 4. |l|+|p|+|η|+|h||l|+|p|+|\eta|+|h| as small as possible for maximized contribution under the Λ^k1\hat{\Lambda}_{k}\ll 1 assumption. One then has, the dominant contribution comes from l=1,p=0,η=1,h=0l=1,p=0,\eta=-1,h=0 or l=1,p=0,η=0,h=1l=1,p=0,\eta=0,h=-1, which gives:

δH1NL¯=\displaystyle\overline{\delta H^{NL}_{1}}= \displaystyle- crB0emEF0,hrδϕ¯2δϕ¯0ω0ω0ωtrωtrω1(ω1ωtr)\displaystyle\frac{c}{rB_{0}}\frac{e}{m}\partial_{E}F_{0,h}\partial_{r}\overline{\delta\phi}_{2^{*}}\overline{\delta\phi}_{0}\frac{\omega_{0}}{\omega_{0}-\omega_{tr}}\frac{\omega_{tr}}{\omega_{1}(\omega_{1}-\omega_{tr})} (18)
×\displaystyle\times J1(Λ^0)J0(Λ^0)J1(Λ^1)J0(Λ^1).\displaystyle J_{1}(\hat{\Lambda}_{0})J_{0}(\hat{\Lambda}_{0})J_{1}(\hat{\Lambda}_{1})J_{0}(\hat{\Lambda}_{1}).

The ratio of thermal ion and EP contribution to the nonlinear coupling, obtained from equations (15) and (18), respectively, can be estimated to be 𝒩i/𝒩h[n0ϵωd,i/ωG]/[Nb(ω0/γ)(ωd,h/ωtr,h)2]Nbϵ/Λh1\mathscr{N}_{i}/\mathscr{N}_{h}\sim[n_{0}\epsilon\omega_{d,i}/\omega_{G}]/[N_{b}(\omega_{0}/\gamma)(\omega_{d,h}/\omega_{tr,h})^{2}]\sim\sqrt{N_{b}}\epsilon/\sqrt{\Lambda_{h}}\ll 1; confirming the conjecture following equation (15). Here, 𝒩i\mathscr{N}_{i} and 𝒩h\mathscr{N}_{h} are, respectively, the thermal ion and EP contribution to nonlinear coupling, respectively. Linear EGAM orderings, including βhβi\beta_{h}\lesssim\beta_{i}, |γ/ωG|Nb|\gamma/\omega_{G}|\sim\sqrt{N_{b}} and ωtr,hωG\omega_{tr,h}\sim\omega_{G} [26] are used in estimating the ordering of 𝒩i/𝒩h\mathscr{N}_{i}/\mathscr{N}_{h}.

Substituting equation (18) into quasi-neutrality condition, one obtains the equation for Ω1\Omega_{1} generation due to Ω0\Omega_{0} and Ω2\Omega_{2^{*}} coupling

1δϕ¯1\displaystyle\mathscr{E}_{1}\overline{\delta\phi}_{1} =\displaystyle= 𝒜𝒟1ω0ω1kr,12rδϕ¯2δϕ¯0.\displaystyle\mathscr{A}\mathscr{D}_{1}\frac{\omega_{0}}{\omega_{1}k^{2}_{r,1}}\partial_{r}\overline{\delta\phi}_{2^{*}}\overline{\delta\phi}_{0}. (19)

Here, 1EGAM(ω1,kr,1)\mathscr{E}_{1}\equiv\mathscr{E}_{EGAM}(\omega_{1},k_{r,1}) is the linear EGAM dispersion relation derived in Ref. [30], which is linearly stable for the GB Ω1\Omega_{1}, with the frequency determined by GAM frequency. Furthermore, 𝒜cΩi2/(rB0n0)\mathscr{A}\equiv c\Omega^{2}_{i}/(rB_{0}n_{0}), and

𝒟1EF0,hω0ωtrωtrω1ωtrJ0(Λ^0)J1(Λ^0)J0(Λ^1)J1(Λ^1).\displaystyle\mathscr{D}_{1}\equiv\left\langle\frac{\partial_{E}F_{0,h}}{\omega_{0}-\omega_{tr}}\frac{\omega_{tr}}{\omega_{1}-\omega_{tr}}J_{0}(\hat{\Lambda}_{0})J_{1}(\hat{\Lambda}_{0})J_{0}(\hat{\Lambda}_{1})J_{1}(\hat{\Lambda}_{1})\right\rangle.

The equation for Ω2\Omega_{2} can be similarly derived as

2δϕ¯2\displaystyle\mathscr{E}_{2^{*}}\overline{\delta\phi}_{2^{*}} =\displaystyle= 𝒜𝒟2ω0ω2kr,22rδϕ¯1δϕ¯0,\displaystyle-\mathscr{A}\mathscr{D}_{2}\frac{\omega^{*}_{0}}{\omega^{*}_{2}k^{2}_{r,2}}\partial_{r}\overline{\delta\phi}_{1}\overline{\delta\phi}_{0^{*}}, (20)

with 2EGAM(ω2,kr,2)\mathscr{E}_{2}\equiv\mathscr{E}_{EGAM}(\omega_{2^{*}},k_{r,2^{*}}) being the dispersion relation of Ω2\Omega_{2^{*}}, and

𝒟2EF0,hω0ωtrωtrω2ωtrJ0(Λ^0)J1(Λ^0)J0(Λ^2)J1(Λ^2).\displaystyle\mathscr{D}_{2}\equiv\left\langle\frac{\partial_{E}F_{0,h}}{\omega^{*}_{0}-\omega_{tr}}\frac{\omega_{tr}}{\omega^{*}_{2}-\omega_{tr}}J_{0}(\hat{\Lambda}_{0})J_{1}(\hat{\Lambda}_{0})J_{0}(\hat{\Lambda}_{2})J_{1}(\hat{\Lambda}_{2})\right\rangle.

The EGAM two plasmon decay dispersion relation can then be derived from equations (19) and (20) as

12=\displaystyle\mathscr{E}_{1}\mathscr{E}_{2^{*}}= \displaystyle- 𝒜2|δϕ0|2|ω0|2ω1ω2kr,1kr,2𝒟1𝒟2.\displaystyle\mathscr{A}^{2}\frac{|\delta\phi_{0}|^{2}|\omega_{0}|^{2}}{\omega_{1}\omega^{*}_{2}k_{r,1}k_{r,2}}\mathscr{D}_{1}\mathscr{D}_{2}. (21)

For the two stable GBs, we have,

11(ω1)+ω11(ω1+iγω0/2)4ω0(iγ+Δ),\displaystyle\mathscr{E}_{1}\simeq\mathscr{E}_{1}(\omega_{1})+\partial_{\omega_{1}}\mathscr{E}_{1}(\omega_{1}+i\gamma-\omega_{0}/2)\simeq\frac{4}{\omega_{0}}(i\gamma+\Delta), (22)

and similarly,

24ω0(iγΔ),\displaystyle\mathscr{E}_{2^{*}}\simeq\frac{4}{\omega^{*}_{0}}(i\gamma-\Delta), (23)

with Δω1ω0/2\Delta\equiv\omega_{1}-\omega_{0}/2 being the mismatch of half primary mode to GBs, and γ\gamma being the secondary mode growth rate due to pump Ω0\Omega_{0} drive. Substituting equations (22) and (23) into (21), we have

γ2+Δ2=14𝒜2|δϕ0|2|ω0|2kr,1kr,2𝒟1𝒟2,\displaystyle\gamma^{2}+\Delta^{2}=-\frac{1}{4}\mathscr{A}^{2}|\delta\phi_{0}|^{2}\frac{|\omega_{0}|^{2}}{k_{r,1}k_{r,2}}\mathscr{D}_{1}\mathscr{D}_{2}, (24)

with the right hand side being the nonlinear EP drive. The secondary modes can be driven unstable as the nonlinear drive overcomes the threshold due to mismatch between half primary mode frequency and GB. Thus, the secondary modes can be excited when the primary amplitude is large enough, or when the frequency mismatch is sufficiently small, i.e., the secondary mode excitation condition is optimized as the primary mode frequency up sweeping to twice local GAM frequency, as observed in the experiment and numerical simulation [37, 39].

If we consider only resonant EP contribution to the nonlinear coupling, taking ωtr,hω0\omega_{tr,h}\simeq\omega_{0}, and assume small EP drift orbit by taking J0(Λ^)1J_{0}(\hat{\Lambda})\simeq 1, J1(Λ^)Λ^/2J_{1}(\hat{\Lambda})\simeq\hat{\Lambda}/2, equation (24) can be reduced to

γ2=Δ2+(π2𝒜)2|δΦ0|2EF0,hρ^d2δ(ω0ωtr)2.\displaystyle\gamma^{2}=-\Delta^{2}+\left(\frac{\pi}{2}\mathscr{A}\right)^{2}|\delta\Phi_{0}|^{2}\left\langle\partial_{E}F_{0,h}\hat{\rho}^{2}_{d}\delta(\omega_{0}-\omega_{tr})\right\rangle^{2}. (25)

It is clear from equation (25) that, the EPs nonlinearly “drive” the secondary modes are the same particles that resonantly drive the primary mode unstable, though the secondary mode frequency is very different from that of the primary mode. Thus, theoretical results from equation (25) illuminate experimental observations as well as the findings from numerical simulations. For more quantitative comparison, the threshold of primary EGAM amplitude for secondary mode generation can be estimated by

|δϕ0|thresholdMax(ΔγG)|π𝒜EF0,hρ^d2δ(ω0ωtr)/2|,\displaystyle|\delta\phi_{0}|_{threshold}\sim\frac{\mbox{Max($\Delta$, $\gamma_{G}$)}}{|\pi\mathscr{A}\langle\partial_{E}F_{0,h}\hat{\rho}^{2}_{d}\delta(\omega_{0}-\omega_{tr})\rangle/2|}, (26)

with γG\gamma_{G} being the GAM collisionless damping rate, and Max(Δ,γG)\mbox{Max}(\Delta,\gamma_{G}) giving the maximum value of Δ\Delta and γG\gamma_{G}.

5 Conclusions and Discussions

In this work, an analytical theory is proposed to interpret the secondary mode generation during primary EGAM frequency chirping observed in LHD experiments [37], which is re-produced in MEGA simulation [39]. The interpretation is based on a previous theory on linear EGAM stability in the same LHD low collisionality plasmas, which shows that for the not fully slowed down EP distribution function, the unstable branch (LBB) frequency can be significantly higher than the local GAM frequency; while there is a linearly stable branch (GB) with the frequency determined by the local GAM frequency. The “primary” and “secondary” modes in the experimental observations [23] correspond to the linearly unstable LBB and linearly stable GB, respectively.

It is shown that, the LBB can decay into to two linearly stable GBs as its frequency is up-chirping to twice GB frequency, in a process similar to the well known two plasmon decay process [42, 43]. The contribution of both thermal plasmas and EPs to the nonlinear process are derived and evaluated. It is found that the thermal plasma contribution to the coupling is negligible compared to that of EP FoWs, and this explains that the nonlinear coupling still occurs when fluid nonlinearity is turned off in the hybrid MEGA simulation. The resonant EPs play crucial roles in the nonlinear coupling, consistent with the observation that the EPs, which “drive” the secondary mode, are the same as those linearly driving the primary mode unstable, though the secondary mode has a frequency much lower than that of the primary. It is noteworthy that the GB frequency is determined by local GAM frequency, and is only slightly modified when GB and LBB strongly couple. Thus, as the primary frequency keeps chirping up, the secondary mode frequency is almost unchanged, as shown in both LHD experimental observation and MEGA simulation. Thus, the present theory, illuminates all the crucial evidence from the experiment and simulation, suggesting this as the mechanism controlling the underlying the physics.

The present theory is local, facilitated by the existence of the high frequency LBB in the low collisionality condition of this specific LHD experiment. However, two plasmon decay process can also occur in typical discharges of usual magnetically confined toroidal plasmas, where the unstable EGAM frequency is typically lower than local GAM frequency. This global two plasmon decay process can occur due to the GAM frequency dependence on local plasma parameters, such that EGAM frequency can be significantly higher than GAM continuum frequency of a distant region, if the temperature gradient is sharp enough. Thus, the two plasmon decay process can occur as the EGAM tunnels through the potential barrier, and strongly couple to GAM where the GAM frequency is half of the EGAM. The condition for the above process to happen is, though, quite difficult to satisfy, since 1. the thermal plasma temperature gradient needs to be sharp, such that the potential barrier is narrow enough to have finite EGAM tunneling through, and 2. the characteristic scale length of thermal plasma temperature nonuniformity needs to be larger than EP density scale length to have EGAM localized by the potential well. The in-depth discussion of the global coupling process is beyond the scope of the present paper focusing on the specific condition of LHD experiments, and will be presented in a separated work.

Acknowledgements

This work is supported by the National Key R&D Program of China under Grant No. 2017YFE0301900, the National Science Foundation of China under grant No. 11875233. This work was also carried out within the framework of the EUROfusion Consortium and received funding from the EURATOM research and training programme 2014 - 2018 and 2019 - 2020 under Grant Agreement No. 633053 (Project Nos. WP19-ER/ENEA-05 and WP17-ER/MPG-01). The views and opinions expressed herein do not necessarily reflect those of the European Commission.

Data Availability

The data that support the findings of this study are available from the corresponding author upon reasonable request.

Appendix A Linear stability of EGAM described by equation (12)

Equation (12) is the linear EGAM dispersion relation excited by a not fully slowed down EP distribution function given by equation (11), with the logarithmic and simple-pole like singularities in the square bracket related to the slowing-down and low energy end cutoff, respectively. The corresponding EGAM linear properties are controlled by three dominant parameters, i.e., ωb\omega_{b} and ωL\omega_{L} determined by NBI birth energy EbE_{b} and low energy end cutoff ELE_{L}, and local GAM frequency ωG\omega_{G}.

Refer to caption
Figure 1: Real frequencies of the three modes dependence on ωL\omega_{L} with ωb=3ωG\omega_{b}=3\omega_{G}. The frequencies are in unites of ωG\omega_{G}.

Here, equation (12) was solved for the EGAM stability v.s. ωL\omega_{L}, given ωb=3ωG\omega_{b}=3\omega_{G} and λ0B0<2/5\lambda_{0}B_{0}<2/5, such that only the simple pole like singularity is destabilizing. Besides, a small but finite GAM damping rate is assumed γG=0.05ωG\gamma_{G}=-0.05\omega_{G}. Note that ωL=ωb\omega_{L}=\omega_{b} corresponds to all the EPs having the same energy; i.e., to beam ions having not slowed down at all; while ωLωb\omega_{L}\ll\omega_{b} (more precisely, Eb>ELEcritE_{b}>E_{L}\gg E_{crit}) corresponds to NBI being fully slowed down. The dependence of the real frequencies of the three branches on ωL\omega_{L} is given in Fig. 1, while their growth rates are given in Fig. 2, with the frequencies/growth rates normalized with ωG\omega_{G}. It is shown that, UBB frequency is determined by ωb\omega_{b} while it remains almost independent of ωG\omega_{G} or ωL\omega_{L}, and it is marginally stable. The LBB frequency is determined by ωL\omega_{L}, and it can be unstable even when its frequency is significantly higher than local GAM frequency. The GB frequency is determined by local GAM frequency, and is almost independent of ωL\omega_{L}.

Refer to caption
Figure 2: Growth rates of the three modes dependence on ωL\omega_{L} with ωb=3ωG\omega_{b}=3\omega_{G}.

The important information here is that, 1. LBB frequency is determined by ωL2EL(1λ0B0)/(qR0)\omega_{L}\equiv\sqrt{2E_{L}(1-\lambda_{0}B_{0})}/(qR_{0}) and the unstable LBB frequency can be significantly higher than local GAM frequency if strongly driven; and 2. GB frequency is determined by local GAM frequency, and its dependence on ωL\omega_{L} is very weak. These two points are crucial for the interpretation of the nonlinear process in Sec. 4.

Appendix B Self-consistent EGAM frequency chirping due to pitch angle scattering

The nonlinear evolution of EGAM including frequency chirping, can be derived by self-consistently including the slowly evolution of the “equilibrium” EP distribution function F0,hF_{0,h} due to the nonlinear interactions with EGAM [10, 9], as addressed in Ref. [18]. The corresponding F0,hF_{0,h} evolution obeys the following Dyson equation [10, 9, 51, 52]

ω^F^0,h\displaystyle\hat{\omega}\hat{F}_{0,h} =\displaystyle= e2ω^d16|δϕG|2E[ω^d(ω^iγ)(ω^iγ)2(ω0,Rωtr,h)2]EF^0,h(ω^2iγ)\displaystyle-\frac{e^{2}\hat{\omega}_{d}}{16}|\delta\phi_{G}|^{2}\frac{\partial}{\partial E}\left[\frac{\hat{\omega}_{d}(\hat{\omega}-i\gamma)}{(\hat{\omega}-i\gamma)^{2}-(\omega_{0,R}-\omega_{tr,h})^{2}}\right]\frac{\partial}{\partial E}\hat{F}_{0,h}(\hat{\omega}-2i\gamma) (27)
+iF0,h(0).\displaystyle+iF_{0,h}(0).

Here, ω^\hat{\omega} denotes the slow nonlinear evolution of F0,hF_{0,h} from its initial value F0,h(0)F_{0,h}(0), F^0,h\hat{F}_{0,h} is the Laplace transform of F0,hF_{0,h}, and ω0,R\omega_{0,R} is the real frequency of EGAM. Equation (27) describes the self-consistent evolution of F0,hF_{0,h}, due to emission and re-absorption of a single coherent EGAM. In deriving equation (27), only evolution in EE (or vv_{\parallel} or λ\lambda) is considered, since both PϕP_{\phi} and μ\mu are well conserved for GAM/EGAM with n=0n=0 and frequency significantly lower than Ωi\Omega_{i}. Equation (27) is derived assuming well circulating EPs and Λ^k1\hat{\Lambda}_{k}\ll 1, while a more systematic treatment can be done following Ref. [10].

EGAM may scatter EPs to smaller pitch angle, and thus, larger ωtr,h\omega_{tr,h} regime, which will lead to self-consistent EGAM frequency up-chirping as its frequency is nonperturbatively determined by ωL\omega_{L}, as we shown in A. However, the self-consistent EGAM evolution will be only qualitatively but not quantitatively investigated in the present work, since it will be addressed in an independent work.

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