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The Velocity-Space Signature of Transit-Time Damping

Rui Huang Email address for correspondence: rui-huang@uiowa.edu Department of Physics and Astronomy, University of Iowa, IA 52242, USA Gregory G. Howes Department of Physics and Astronomy, University of Iowa, IA 52242, USA Andrew J. McCubbin Applied Physics Laboratory, Johns Hopkins University, MD 20723, USA
(2024; ?; revised ?; accepted ?. - To be entered by editorial office)
Abstract

Transit-time damping (TTD) is a process in which the magnetic mirror force—induced by the parallel gradient of magnetic field strength—interacts with resonant plasma particles in a time-varying magnetic field, leading to the collisionless damping of electromagnetic waves and the resulting energization of those particles through the perpendicular component of the electric field, EE_{\perp}. In this study, we utilize the recently developed field-particle correlation technique to analyze gyrokinetic simulation data. This method enables the identification of the velocity-space structure of the TTD energy transfer rate between waves and particles during the damping of plasma turbulence. Our analysis reveals a unique bipolar pattern of energy transfer in velocity space characteristic of TTD. By identifying this pattern, we provide clear evidence of TTD’s significant role in the damping of strong plasma turbulence. Additionally, we compare the TTD signature with that of Landau damping (LD). Although they both produce a bipolar pattern of phase-space energy density loss and gain about the parallel resonant velocity of the Alfvénic waves, they are mediated by different forces and exhibit different behaviors as v0v_{\perp}\to 0. We also explore how the dominant damping mechanism varies with ion plasma beta βi\beta_{i}, showing that TTD dominates over LD for βi>1\beta_{i}>1. This work deepens our understanding of the role of TTD in the damping of weakly collisional plasma turbulence and paves the way to seek the signature of TTD using in situ spacecraft observations of turbulence in space plasmas.

volume: ?
{PACS}

1 Introduction

A key area of research in the study of turbulence in weakly collisional plasmas is understanding how energy from the fluctuating plasma flows and electromagnetic fields is converted into plasma particle energy. This phenomenon is especially relevant in heliospheric plasmas like the solar wind, where the characteristic low density and high temperature lead to weakly collisional plasma dynamics. The dissipation of turbulence in such space and astrophysical plasmas is likely mediated by three categories of mechanisms: (i) resonant wave-particle interactions, such as Landau damping (Landau, 1946; Chen et al., 2019), transit-time damping (Stix, 1992; Barnes, 1966), and cyclotron damping (Isenberg & Hollweg, 1983; Isenberg & Vasquez, 2019); (ii) non-resonant wave-particle interactions, including stochastic heating (Chandran et al., 2010, 2013; Martinović et al., 2020; Cerri et al., 2021), magnetic pumping (Lichko & Egedal, 2020; Montag & Howes, 2022), and “viscous” damping mediated by kinetic temperature anisotropy instabilities (Arzamasskiy et al., 2023); and (iii) dissipation within coherent structures, in particular collisionless magnetic reconnection that may occur in current sheets that are found to arise naturally in plasma turbulence (Osman et al., 2011; Zhdankin et al., 2015; Mallet et al., 2017; Loureiro & Boldyrev, 2017).

Given the low collisionality of these plasma environments, the six-dimensional (3D-3V) kinetic plasma theory is essential for analyzing the evolution of the turbulence and its dissipation through collisionless interactions between electromagnetic fields and plasma particles (Howes, 2017). Although in situ spacecraft measurements in the solar wind provide invaluable data, they are often limited to a single point, or a few points, in space, which presents a significant challenge for the investigation of the physical mechanisms that remove energy from the turbulent fluctuations and consequently energize the plasma particles. The recently developed field–particle correlation technique (Klein & Howes, 2016; Howes et al., 2017; Klein et al., 2017) enables direct measurements of the electromagnetic fields and particle velocity distributions at a single point in space to be combined to create a velocity-space signature of particle energization that can be used to identify the physical mechanisms responsible for damping the turbulence and to estimate the resulting rate of the change of particle energy density. Consequently, this technique provides an innovative means to utilize in situ spacecraft observations to identify specific collisionless damping mechanisms and determine particle heating rates.

This technique has shown success in identifying several damping mechanisms in weakly collisional turbulent plasmas, such as ion Landau damping (Klein et al., 2017; Li et al., 2019), ion cyclotron damping (Klein et al., 2020; Afshari et al., 2023), electron Landau damping (Chen et al., 2019; Li et al., 2019; Afshari et al., 2021; Conley et al., 2023), and magnetic pumping (Montag & Howes, 2022). However, the role of transit-time damping, a resonant wave-particle interaction, in the damping of plasma turbulence remains unconfirmed. The focus of this paper is to employ the field-particle correlation technique to identify the velocity-space signature of ion energization through transit-time damping and to recover this signature from simulations of strong plasma turbulence.

The structure of this paper is laid out as follows. We derive the specific form of the field-particle correlation for transit-time damping in §2.1. This is followed by an exploration of the expected transit-time damping signature in §2.2. In §3, we conduct single kinetic Alfvén wave simulations to investigate the velocity-space signature characteristic of transit-time damping. Subsequently, in §4, we delve into turbulence simulations, presenting details for distinguishing transit-time damping from turbulence damping process. §5 summarizes our findings and outlines potential future applications for further research.

2 Transit-Time Damping

The idea of transit-time damping (TTD) had its origins in mid-20th-century plasma physics when transit-time magnetic pumping was proposed as a means to heat confined plasma (Spitzer Jr & Witten, 1953). This method is characterized by a modulation of the magnetic field magnitude at a frequency considerably lower than the ion cyclotron frequency; the evolution of the parallel and perpendicular particle velocities in the time-varying magnetic field, combined with a weak collisionality, leads to a net transfer of energy to the plasma particles. The term “transit-time” refers to the duration necessary for an ion to traverse from one side to the other across the confined region.

The magnetic mirror force plays a key role in the dynamics of TTD. In a static magnetic field with a spatial variation of the magnetic field magnitude along the direction parallel to the field, the mirror force accelerates charged particles in the direction of decreasing field magnitude. In a cylindrical coordinate system aligned with the magnetic field direction, the condition 𝑩=0\nabla\cdot\bm{B}=0 implies that an increase of the magnetic field along the axial direction must be accompanied by the convergence of the field in the radial direction, as shown in Figure 1. For a particle with a guiding center on the axis, the particle will experience an inward radial field throughout its Larmor orbit. The Lorentz force, which acts perpendicularly to the magnetic field direction at the particle position, will therefore have both a large radial and a small axial component. Averaged over the full Larmor orbit, the net nonzero axial component accelerates the particle in the direction of the decreasing magnetic field magnitude. Because the magnetic field can do no work, the total energy of the particle remains constant—the change in the parallel velocity is accompanied by a small change in the perpendicular velocity governed by the average of the radial component of the Lorentz force. The net effect of the magnetic mirror force is that, as a particle moves in the direction of the increasing magnetic field, the mirror force reduces the velocity vv_{\parallel} parallel to the mean magnetic field over the Larmor orbit and increases perpendicular velocity vv_{\perp} to maintain a constant total velocity v=(v2+v2)1/2v=(v^{2}_{\perp}+v^{2}_{\parallel})^{1/2}.

Refer to caption
Figure 1: Diagram of the radial component FrF_{r} and axial component FzF_{z} of the Lorentz force of the magnetic field (red) on a positively charged particle (red ++) in a converging magnetic field (green) with increasing magnitude in the +z+z direction. Averaged over the Larmor orbit of the particle (blue), the net magnetic mirror force is in the direction of decreasing magnetic field magnitude, here the z-z direction.

Although the mirror force in a static magnetic field cannot change the energy of particles, any changes of the magnetic field in time will induce an electric field according to Faraday’s Law. Work done by that induced electric field can do work on the particles, providing the key element underlying the physics of TTD. In a collisionless plasma, collisionless wave-particle interactions are governed by the resonance condition, given by ωkv=nΩs\omega-k_{\parallel}v_{\parallel}=n\Omega_{s}, where nΩsn\Omega_{s} for n=0,±1,±2,n=0,\pm 1,\pm 2,\ldots incorporates the cyclotron harmonics of the particle motion in a magnetic field (Melrose, 1980). Here we adopt the convention that the value of ω\omega is positive, so that the sign of 𝒌\bm{k} indicates the direction of the phase velocity. The n=0n=0 resonance, known as the Landau resonance, describes resonant interactions with particles that have parallel velocities near the phase velocity of the wave, vω/kv_{\parallel}\simeq\omega/k_{\parallel}, enabling energy exchange between the particles and the wave through two mechanisms: (i) the electrostatic force due to the parallel component of the electric field governing the phenomenon of Landau damping (LD) (Landau, 1946; Villani, 2014); (ii) the magnetic mirror force governing the phenomenon of TTD (Stix, 1992), also known as Barnes damping (Barnes, 1966). In the case of TTD, the perpendicular component of the electric field, induced by the change in the magnetic field magnitude along the parallel direction, accelerates the particle by changing the perpendicular velocity vv_{\perp}; the mirror force effectively converts this perpendicular velocity into parallel velocity, leading to a net acceleration of the particle along the axial direction parallel to the magnetic field (Howes et al., 2024). For a Maxwellian distribution of particles, there are more particles with parallel velocities |v|<ω/|k||v_{\parallel}|<\omega/|k_{\parallel}| than particles with |v|>ω/|k||v_{\parallel}|>\omega/|k_{\parallel}|, so the net effect on the distribution is an increase of the particle energy, leading to damping of the wave. A detailed demonstration of this phenomenon for a model moving magnetic mirror field is presented in §2.2.

2.1 Field-Particle Correlation for Transit-Time Damping

To determine the appropriate form of the field-particle correlation to diagnose TTD via the magnetic mirror force, we start with the Vlasov equation for a species ss being acted upon by a general force 𝑭s\bm{F}_{s},

fst+𝒗fs+𝑭smsfs𝒗=0.\frac{\partial f_{s}}{\partial t}+\bm{v}\cdot\nabla f_{s}+\frac{\bm{F}_{s}}{m_{s}}\cdot\frac{\partial f_{s}}{\partial\bm{v}}=0. (1)

Multiplying the Vlasov equation by msv2/2m_{s}v^{2}/2, we obtain an expression for the rate of change of the phase-space energy density, ws(𝒓,𝒗,t)msv2fs(𝒓,𝒗,t)/2w_{s}(\bm{r},\bm{v},t)\equiv m_{s}v^{2}f_{s}(\bm{r},\bm{v},t)/2,

ws(𝒓,𝒗,t)t=𝒗wsv22𝑭sfs𝒗.\frac{\partial w_{s}(\bm{r},\bm{v},t)}{\partial t}=-\bm{v}\cdot\nabla w_{s}-\frac{v^{2}}{2}\bm{F}_{s}\cdot\frac{\partial f_{s}}{\partial\bm{v}}. (2)

Previous analysis of this equation (Klein & Howes, 2016; Howes et al., 2017) has shown that, if integrated over space (with appropriate infinite or periodic boundary conditions), the change in the total kinetic energy of the particles 𝔚s(t)=d3𝒓d3𝒗ws(𝒓,𝒗,t)\mathfrak{W}_{s}(t)=\int d^{3}\bm{r}\int d^{3}\bm{v}\ w_{s}(\bm{r},\bm{v},t) is due to work done on the particle species by the force 𝑭s\bm{F}_{s}. Therefore, the field-particle correlation due to a general force 𝑭s\bm{F}_{s} at spatial position 𝒓0\bm{r}_{0} is defined as a time-average over a correlation interval τ\tau of the last term on the right hand side of (2),

C𝑭s(𝒓0,𝒗,t;τ)1τtτ/2t+τ/2v22𝑭s(𝒓0,𝒗,t)fs(𝒓0,𝒗,t)𝒗𝑑t.C_{\bm{F}_{s}}(\bm{r}_{0},\bm{v},t;\tau)\equiv\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}\frac{-v^{2}}{2}\bm{F}_{s}(\bm{r}_{0},\bm{v},t^{\prime})\cdot\frac{\partial f_{s}(\bm{r}_{0},\bm{v},t^{\prime})}{\partial\bm{v}}dt^{\prime}. (3)

Note here that the correlation interval τ\tau is a parameter of the field-particle correlation analysis, and so is included as a secondary argument, separated by a semicolon from the primary arguments that define the dimensions of the 3D-3V phase space in position, velocity, and time.

If we consider the force due to an electric field 𝑭s=qs𝑬\bm{F}_{s}=q_{s}\bm{E}, we obtain the established field-particle correlation due to the electric field (Klein & Howes, 2016; Howes et al., 2017; Klein et al., 2017),

C𝑬,s(𝒓0,𝒗,t;τ)=1τtτ/2t+τ/2qsv22𝑬(𝒓0,t)fs(𝒓0,𝒗,t)𝒗𝑑t.C_{\bm{E},s}(\bm{r}_{0},\bm{v},t;\tau)=\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}\frac{-q_{s}v^{2}}{2}\bm{E}(\bm{r}_{0},t^{\prime})\cdot\frac{\partial f_{s}(\bm{r}_{0},\bm{v},t^{\prime})}{\partial\bm{v}}dt^{\prime}. (4)

The collisionless transfer of energy between electromagnetic waves and particles in TTD is mediated by the magnetic mirror force, 𝑭s=μs𝒃^𝑩\bm{F}_{s}=-\mu_{s}\mbox{$\hat{\bm{b}}$}\cdot\nabla\bm{B}, where the magnetic moment for a particle of species ss is given by μs=msv2/(2B)\mu_{s}=m_{s}v_{\perp}^{2}/(2B), the unit vector in the direction of the magnetic field is given by 𝒃^𝑩/B\mbox{$\hat{\bm{b}}$}\equiv\bm{B}/B, and the magnitude of the magnetic field is B=|𝑩|B=|\bm{B}|. Substituting the magnetic mirror force into (3), we obtain

C𝑩,s(𝒓0,𝒗,t;τ)=1τtτ/2t+τ/2msv2v24B(𝒃^)𝑩(𝒓0,t)fs(𝒓0,𝒗,t)𝒗𝑑t.C_{\bm{B},s}(\bm{r}_{0},\bm{v},t;\tau)=\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}\frac{m_{s}v^{2}v_{\perp}^{2}}{4B}(\mbox{$\hat{\bm{b}}$}\cdot\nabla)\bm{B}(\bm{r}_{0},t^{\prime})\cdot\frac{\partial f_{s}(\bm{r}_{0},\bm{v},t^{\prime})}{\partial\bm{v}}dt^{\prime}. (5)

A few modifications of the form of the field-particle correlation for TTD given in (5) are helpful for its application to the gyrokinetic simulations presented here. First, we exploit two important characteristics of TTD and turbulence: (i) TTD is most effective in damping the dominant Alfvénic fluctuations111This peak in TTD damping rates is clearly shown in the linear dispersion relation plots for the Alfvén wave mode shown in Figure 6. in turbulence with perpendicular wavelengths at the ion scales, kρikρi1k_{\perp}\rho_{i}\sim k\rho_{i}\sim 1 where k/k1k_{\parallel}/k_{\perp}\ll 1; and (ii) for most turbulent space and astrophysical plasmas of interest, the amplitude of the magnetic fluctuations δ𝑩\delta\bm{B} at ion scales kρi1k\rho_{i}\sim 1 is much smaller than the magnitude of the mean magnetic field 𝑩0\bm{B}_{0}. Therefore, if we separate the magnetic field into its mean plus the fluctuations, 𝑩=𝑩0+δ𝑩\bm{B}=\bm{B}_{0}+\delta\bm{B}, where |δ𝑩||𝑩0||\delta\bm{B}|\ll|\bm{B}_{0}|, the change in the magnetic field magnitude δ|𝑩|\delta|\bm{B}| (which is the key ingredient for the magnetic mirror force) can be expressed as δB\delta B_{\parallel} by recognizing

δ|𝑩|=|𝑩||𝑩0|=(𝑩0+δ𝑩)2B0=B02+2δ𝑩𝑩0+|δ𝑩|2B0δB\delta|\bm{B}|=|\bm{B}|-|\bm{B}_{0}|=\sqrt{(\bm{B}_{0}+\delta\bm{B})^{2}}-B_{0}=\sqrt{B_{0}^{2}+2\delta\bm{B}\cdot\bm{B}_{0}+|\delta\bm{B}|^{2}}-B_{0}\simeq\delta B_{\parallel} (6)

where we use a binomial expansion to eliminate the square root, neglect the small |δ𝑩|2|\delta\bm{B}|^{2} term, and write δB=δ𝑩(𝑩0/B0)\delta B_{\parallel}=\delta\bm{B}\cdot(\bm{B}_{0}/B_{0}) as the variation in the component of the perturbed magnetic field parallel to the mean magnetic field. Furthermore, separating term v2=v2+v2v^{2}=v_{\perp}^{2}+v_{\parallel}^{2} in the correlation (5), it is easy to show that the v2v_{\perp}^{2} contribution yields a perfect differential in fsf_{s} when integrated over all parallel velocity (Howes et al., 2017), so we choose to omit this term since it leads to zero net change in the particle energy. Finally, we write the gradient along the magnetic field direction by 𝒃^\nabla_{\parallel}\equiv\mbox{$\hat{\bm{b}}$}\cdot\nabla, leading to our preferred form of the field-particle correlation for TTD,

CδB,s(𝒓0,𝒗,t;τ)=1τtτ/2t+τ/2msv2v24BδBfs(𝒓0,𝒗,t)vdt.C_{\delta B_{\parallel},s}(\bm{r}_{0},\bm{v},t;\tau)=\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}\frac{m_{s}v_{\parallel}^{2}v_{\perp}^{2}}{4B}\nabla_{\parallel}\delta B_{\parallel}\frac{\partial f_{s}(\bm{r}_{0},\bm{v},t^{\prime})}{\partial v_{\parallel}}dt^{\prime}. (7)

In the gyrokinetic system of equations (Antonsen Jr & Lane, 1980; Frieman & Chen, 1982; Howes et al., 2006; Schekochihin et al., 2009), the gyro-averaged effect of parallel magnetic field gradients leads to the magnetic mirror force, which can accelerate particles in the direction parallel to the magnetic field via the Landau resonance, and therefore can lead to collisionless TTD of electromagnetic fluctuations. A rigorous derivation of the gyrokinetic equation in Appendix A shows explicitly the two collisionless wave-particle interactions via the Landau resonance—specifically, LD and TTD. The natural form of the field-particle correlation arising from the gyrokinetic version of the generalized energy density equation is slightly different from the field-particle correlation for TTD given in (7), but the gyrokinetic form requires the gyroaveraged distribution function, which is not accessible through single-point spacecraft measurements and is not a natural quantity that can easily be derived from other kinetic simulation approaches, such as particle-in-cell or Vlasov simulations. Therefore, we choose here to use the perturbed distribution functions and electromagnetic fields generated by our gyrokinetic simulations, but we analyze them using (7) which is more directly applicable to spacecraft measurements or alternative kinetic simulation approaches, such as particle-in-cell codes.

Utilizing the gyroaveraged distribution function and corresponding fields, the quantity CδB,s(𝒓0,𝒗,t;τ)C_{\delta B_{\parallel},s}(\bm{r}_{0},\bm{v},t;\tau) reveals the velocity-space signature of TTD on the gyrotropic velocity space (v,v)(v_{\perp},v_{\parallel}). To simplify the notation, henceforth we shall employ CδB,s(v,v)C_{\delta B_{\parallel},s}(v_{\parallel},v_{\perp}) to signify the gyrotropic correlation, explicitly noting the associated spatial position 𝒓0\bm{r}_{0}, time tt, and the correlation interval τ\tau only when necessary. The resonant structure of the velocity-space signature of TTD is primarily a function of vv_{\parallel}, so it is often useful to define the reduced parallel field-particle correlation by integrating CδB,s(v,v,t)C_{\delta B_{\parallel},s}(v_{\parallel},v_{\perp},t) over vv_{\perp}, given by CδB,s(v,t)2πCδB,s(v,v,t)v𝑑vC_{\delta B_{\parallel},s}(v_{\parallel},t)\equiv 2\pi\int C_{\delta B_{\parallel},s}(v_{\parallel},v_{\perp},t)v_{\perp}dv_{\perp}, where the extra 2πv2\pi v_{\perp} factor arises from the integration over the gyrophase in 3V phase space. A timestack plot of the reduced parallel correlation CδB,s(v,t)C_{\delta B_{\parallel},s}(v_{\parallel},t) reveals the persistence in time of any resonant velocity-space signatures in vv_{\parallel}. We can also consider the rate of change of the kinetic energy density of species ss due to TTD by integrating the gyrotropic correlation over all velocity space: (Ws/t)TTD=CδB,s(v,v)d3𝒗(\partial W_{s}/\partial t)_{\mbox{TTD}}=\int C_{\delta B_{\parallel},s}(v_{\parallel},v_{\perp})d^{3}\bm{v}.

In closing, note that the gyroaveraging procedure employed in the derivation of the system of gyrokinetics enables the variations in the perpendicular components of the electric field EE_{\perp} to be expressed in terms of changes in the parallel component of the magnetic field δB\delta B_{\parallel}, as shown by (17). In a system where the gyroaverage has not been performed, the work done by TTD is actually mediated (at the position of the particle) by the perpendicular component of the electric field EE_{\perp} (Howes et al., 2024). Therefore, the perpendicular electric field correlation, given by summing the two perpendicular contributions to the electric field correlation, CE(𝒓0,𝒗,t;τ)C_{E_{\perp}}(\bm{r}_{0},\bm{v},t;\tau) (Klein et al., 2020; Afshari et al., 2023), can be used to seek the velocity-space signature of TTD at the parallel resonant phase velocity, as seen recently in hybrid particle-in-cell simulations of plasma turbulence (Cerri et al., 2021).

2.2 Prediction of the Velocity-Space Signature of Transit-Time Damping

To predict the velocity-space signature of TTD, we begin with a simple model of a magnetic field with an amplitude variation that varies along the mean field direction zz, given in cylindrical coordinates (r,ϕ,z)(r,\phi,z) by

𝑩(r,ϕ,z)=δBz4krsin(kz)𝒓^+{B0+δBz2[1cos(kz)]}𝒛^\bm{B}(r,\phi,z)=-\frac{\delta B_{z}}{4}kr\sin(kz^{\prime})\hat{\bm{r}}+\left\{B_{0}+\frac{\delta B_{z}}{2}[1-\cos(kz^{\prime})]\right\}\hat{\bm{z}}\\ (8)

where the wavenumber kk of the spatial variation of the magnetic field magnitude is along the mean field direction zz, and z=zUtz^{\prime}=z-Ut, such that that pattern moves in the +z+z direction with a phase speed U0U\geq 0. The corresponding electric field variation can be determined by the Lorentz transform222The equations for spatial and temporal variations of the magnetic and electric field given by (8) and (9) satisfy Faraday’s Law, indicating explicitly that the electric field arises from the time variation of the magnetic field, but mathematically solving for (9) is more easily done using the Lorentz transform. from the primed (wave) frame KK^{\prime} in which the magnetic field pattern is stationary (and therefore 𝑬=0\bm{E}^{\prime}=0) to the unprimed (lab) frame KK. This Lorentz transformation in the non-relativistic limit U/c1U/c\ll 1 is given by 𝑬=𝑬𝑼×𝑩\bm{E}=\bm{E}^{\prime}-\bm{U}\times\bm{B} and 𝑩=𝑩\bm{B}=\bm{B}^{\prime} (Howes et al., 2014), where the transformation velocity is just 𝑼=U𝒛^\bm{U}=U\mbox{$\hat{\bm{z}}$}. The resulting induced electric field in the lab frame KK is given by

𝑬(r,ϕ,z)=UδBz4krsin(kz)ϕ^.\bm{E}(r,\phi,z)=U\frac{\delta B_{z}}{4}kr\sin(kz^{\prime})\hat{\bm{\phi}}.\\ (9)

With this simple model, we can illustrate how a single particle is accelerated into different regions of velocity space by the electromagnetic fields. Extending this approach to consider a distribution of particles will enable us to predict the qualitative and quantitative features of the velocity-space signature of TTD.

Consider first the acceleration of a single particle in a stationary mirror field with U=0U=0, as shown in Figure 2(a), for a “wave” amplitude of δBz/B0=0.2\delta B_{z}/B_{0}=0.2, giving a mirror ratio of Bmax/Bmin=1.2B_{\text{max}}/B_{\text{min}}=1.2. The particle begins at the minimum in the magnetic field at z=0z=0 with an initial perpendicular velocity vv_{\perp} and an initial parallel velocity v<0v_{\parallel}<0, given by the red ++ in the figure at the tip of the initial velocity vector 𝒗i\bm{v}_{i} (blue). As the particle moves into the increasing magnetic field at z<0z<0, the mirror force increases vv_{\perp} and decreases vv_{\parallel} such that the particle moves through velocity space (green arrow) on a circle of constant total velocity v=v2+v2v=\sqrt{v_{\parallel}^{2}+v_{\perp}^{2}} (black dashed circle). The particle will be reflected by the mirror field if the particle has an initial pitch angle α=tan1(v/v)\alpha=\tan^{-1}(v_{\perp}/v_{\parallel}) larger than the loss cone angle αloss=sin1(Bmin/Bmax)\alpha_{\mbox{loss}}=\sin^{-1}\left(\sqrt{B_{\text{min}}/B_{\text{max}}}\right). For Bmax/Bmin=1.2B_{\text{max}}/B_{\text{min}}=1.2, the loss cone angle is αloss=66\alpha_{\mbox{loss}}=66^{\circ}; the particle depicted in Figure 2(a) has an initial pitch angle α>αloss\alpha>\alpha_{\mbox{loss}} and is therefore reflected by the mirror field. The particle follows this circular trajectory in (v,v)(v_{\parallel},v_{\perp}) velocity space until it returns to its initial axial position z=0z=0, ending up with a final velocity 𝒗f\bm{v}_{f} (blue) with the same perpendicular component but an equal and opposite parallel component. Thus, the kinetic energy of the particle does not change, consistent with the fact that magnetic fields do no work on particles. The particle has simply been reflected by the mirror, reversing the sign of its parallel velocity.

Next, we consider the case for a magnetic mirror field moving with velocity 𝑼=U𝒛^\bm{U}=U\mbox{$\hat{\bm{z}}$}, where U>0U>0. In the wave frame, moving at velocity 𝑼=U𝒛^\bm{U}=U\mbox{$\hat{\bm{z}}$} in which the magnetic field is stationary, the acceleration of the particle by the magnetic field must be the same as the stationary case in Figure 2(a). But, in the lab frame, depicted in Figure 2(b), the particle now moves on a circular trajectory in velocity space centered about the mirror velocity UU, given by a constant magnitude of velocity in the wave frame v0=(vU)2+v2v_{0}=\sqrt{(v_{\parallel}-U)^{2}+v_{\perp}^{2}}. Here the particle is initially moving in the same direction as the mirror field but with a slower initial parallel velocity 0vU0\leq v_{\parallel}\leq U, given by the red ++ in the figure at the tip of the initial velocity vector 𝒗i\bm{v}_{i} (blue). If the pitch angle in the wave frame αw=tan1[v/(vU)]\alpha_{w}=\tan^{-1}[v_{\perp}/(v_{\parallel}-U)] is greater than the loss-cone angle, αw>αloss\alpha_{w}>\alpha_{\mbox{loss}}, the particle will be reflected by the moving mirror field, leading to a net acceleration in the axial direction, ultimately ending up with a parallel velocity greater than the mirror velocity v>Uv_{\parallel}>U, with a final velocity vector 𝒗f\bm{v}_{f} (blue). In this case, the induced electric field given by (9) has done work on the particle (Howes et al., 2024), ultimately leading to a net acceleration in the axial direction. This process is the fundamental energy transfer underlying the physics of TTD.

Finally, we consider how this understanding of the single particle motion and acceleration can be combined with a distribution of initial particle velocities to predict the velocity-space signature of TTD. Note that for the sinusoidally oscillating magnetic field magnitude given by (8), the long time evolution of the particle in velocity space would oscillate back and forth between 𝒗i\bm{v}_{i} and 𝒗f\bm{v}_{f} along the green trajectory shown in Figure 2(a) and (b); for example, if the particle started with initial velocity 𝒗f\bm{v}_{f}, the other side of the mirror field would lead to a reflection in the opposite direction, ultimately resulting in the particle ending up with a final velocity 𝒗i\bm{v}_{i}. In the case of a moving mirror field, for a Maxwellian velocity distribution there will be more particles with parallel velocities v<Uv_{\parallel}<U than with v>Uv_{\parallel}>U, so the net effect is that more particles will gain energy than lose energy, leading to a net energization of the particles and consequent damping of the electromagnetic wave. Only particles with pitch angles in the wave frame larger than the loss cone angle, αw>αloss\alpha_{w}>\alpha_{\mbox{loss}}, will undergo the mirror reflection, so that net effect on the distribution is an acceleration of particles from v<Uv_{\parallel}<U to v>Uv_{\parallel}>U. The resulting change in the phase-space energy density leads to the prediction of the velocity-space signature of TTD depicted in Figure 2(c): a loss of phase-space energy density (blue) in the region v<Uv_{\parallel}<U, and a gain of phase-space energy density (red) in the region v>Uv_{\parallel}>U. The extent of this velocity-space signature in (v,v)(v_{\parallel},v_{\perp}) velocity space is confined by two effects: (i) only particles outside of the loss cone will experience a net acceleration; and (ii) the signature is weighted by the v2v_{\perp}^{2} weighting in (7) for the rate of change of phase-space energy density by TTD (which arises from the magnetic moment μ=mv2/(2B)\mu=mv_{\perp}^{2}/(2B) dependence of the mirror force) combined with the reduced perpendicular velocity distribution f(v)f(v_{\perp}), where this net weighting of v2f(v)v_{\perp}^{2}f(v_{\perp}) is shown in Figure 2(d). Thus, the velocity-space signature of TTD in Figure 2(c) is restricted to “Landau resonant” particles with parallel velocities near the velocity of the magnetic field pattern vUv_{\parallel}\sim U and to a region away from the v=0v_{\perp}=0 axis, unlike the velocity-space signature of LD (Klein & Howes, 2016; Howes et al., 2017; Klein et al., 2017) which extends down to v=0v_{\perp}=0.

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(a)                                                   (b)

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(c)                                                                     (d)

Figure 2: Diagram of the magnetic mirror force and prediction for the velocity-space signature of TTD: (a) vv_{\perp} versus vv_{\parallel} for the single particle motion in a static magnetic mirror field; (b) vv_{\perp} versus vv_{\parallel} for the single particle motion in a moving magnetic mirror field, where the vertical black dashed line denotes the wave phase velocity UU; (c) the predicted velocity-space signature for a Maxwellian velocity distribution function, where the phase-space energy density decreases at v<Uv_{\parallel}<U (blue) and increases at v>Uv_{\parallel}>U (red); (d) effective vv_{\perp} weighting of correlation v2f(v)v_{\perp}^{2}f(v_{\perp}), which constrains the velocity-space signature in the vv_{\perp} direction.

3 Single Kinetic Alfvén Wave (KAW) Simulations

Here we perform numerical simulations of single kinetic Alfvén waves to determine the velocity-space signature of TTD using the Astrophysical Gyrokinetics Code, AstroGK (Numata et al., 2010). AstroGK evolves the gyroaveraged scalar potential ϕ(𝒓)\phi(\bm{r}), parallel vector potential A(𝒓)A_{\parallel}(\bm{r}), and the parallel magnetic field fluctuation δB(𝒓)\delta B_{\parallel}(\bm{r}), as well as the gyrokinetic distribution function hs(𝒓,v,v)h_{s}(\bm{r},v_{\perp},v_{\parallel}), in a triply-periodic slab geometry of size L2×LL_{\perp}^{2}\times L_{\parallel} elongated along the straight, uniform mean magnetic field 𝑩0=B0𝒛^\bm{B}_{0}=B_{0}\mbox{$\hat{\bm{z}}$}. The domain-scale wavenumbers are defined by k0=2π/Lk_{\parallel 0}=2\pi/L_{\parallel} and k0=2π/Lk_{\perp 0}=2\pi/L_{\perp}. The gyrokinetic expansion parameter is defined by ϵk0/k01\epsilon\sim k_{\parallel 0}/k_{\perp 0}\ll 1 (Howes et al., 2006), and all quantities are scaled to accommodate an arbitrary value of ϵ\epsilon. The gyrokinetic distribution function is related to the total distribution function fsf_{s} via

fs(𝒓,𝒗,t)=F0s(v)(1qsϕ(𝒓,t)Ts)+hs(𝑹s,v,v,t)+δf2s+f_{s}(\bm{r},\bm{v},t)=F_{0s}(v)\left(1-\frac{q_{s}\phi(\bm{r},t)}{T_{s}}\right)+{h_{s}}(\bm{R}_{s},v_{\perp},v_{\parallel},t)+\delta f_{2s}+... (10)

where F0sF_{0s} is the equilibrium distribution, 𝒓\bm{r} is the spatial position, 𝑹s\bm{R}_{s} is the associated species gyrocenter related to 𝒓\bm{r} by 𝒓=𝑹s𝒗×𝒛^/Ωs\bm{r}=\bm{R}_{s}-\bm{v}\times\mbox{$\hat{\bm{z}}$}/\Omega_{s}, and δf2s\delta f_{2s} are corrections second-order in the gyrokinetic expansion parameter ϵ\epsilon which are not retained (Howes et al., 2006). The code employs a pseudospectral method in the (x,y)(x,y) (perpendicular) plane and finite differencing in the zz-direction. The velocity distribution is resolved on a grid in energy E=v2+v2E=v_{\parallel}^{2}+v_{\perp}^{2} and pitch angle λ=v2/v2\lambda=v^{2}_{\perp}/v^{2} space, with the points selected on a Legendre polynomial basis. A fully conservative, linearized, gyroaveraged collision operator is employed (Abel et al., 2008; Barnes et al., 2009) to ensure velocity-space structure in hsh_{s} remains resolved throughout the simulation evolution. We normalize time using the domain-scale Alfvén wave frequency ωAk0vA\omega_{A}\equiv k_{\parallel 0}v_{A}, and particle velocity is normalized to the ion thermal velocity vti=2Ti/miv_{\text{ti}}=\sqrt{2T_{i}/m_{i}}, where the Boltzmann constant has been absorbed to yield temperature in units of energy.

3.1 Single Wave Simulation Set Up

We first determine the velocity-space signature of TTD by performing simulations of single kinetic Alfvén waves (KAWs) for a fully ionized proton-electron plasma with Maxwellian equilibrium velocity distributions with a temperature ratio Ti/Te=1T_{i}/T_{e}=1 and a realistic ion-to-electron mass ratio of mi/me=1836m_{i}/m_{e}=1836. We perform three simulations with ion plasma beta βi=0.3,1,3\beta_{i}=0.3,1,3 and sample the time evolution of the electromagnetic fields and gyrokinetic distribution function at discrete single points throughout the simulation domain with dimensions L=2πρiL_{\perp}=2\pi\rho_{i} and L=2πa0L_{\parallel}=2\pi a_{0}, yielding an arbitrary expansion parameter ϵ=ρi/a01\epsilon=\rho_{i}/a_{0}\ll 1. The ion plasma beta is defined by βi=8πniTi/B2=vti2/vA2\beta_{i}=8\pi n_{i}T_{i}/B^{2}=v_{ti}^{2}/v_{A}^{2}, where the ion thermal velocity is vti=2Ti/miv_{ti}=\sqrt{2Ti/m_{i}}, the Alfvén velocity is vA=B/4πnimiv_{A}=B/\sqrt{4\pi n_{i}m_{i}}, and the Boltzmann constant is absorbed to give temperature in units of energy. Here ρivti/Ωi\rho_{i}\equiv v_{ti}/\Omega_{i} is the ion Larmor radius, where the angular ion (proton) cyclotron frequency is Ωi=qiB0/mi\Omega_{i}=q_{i}B_{0}/m_{i}. The dimensions of these single-wave simulations are (nx,ny,nz,nλ,nE,ns)=(10,10,32,128,64,2)(n_{x},n_{y},n_{z},n_{\lambda},n_{E},n_{s})=(10,10,32,128,64,2), where nsn_{s} denotes the number of species. Using the solutions to the linear gyrokinetic dispersion relation (Howes et al., 2006), a single plane-wave KAW with wavevector (kxρi,kyρi,ka0)=(1,0,1)(k_{x}\rho_{i},k_{y}\rho_{i},k_{\parallel}a_{0})=(1,0,1) and amplitude333Note that the gyrokinetic simulation results can be scaled to any value of the gyrokinetic expansion parameter, ϵ1\epsilon\ll 1. δB/B0=0.125ϵ\delta B_{\perp}/B_{0}=0.125\epsilon is initialized throughout the domain and allowed to evolve linearly for 5 wave periods with enhanced collisionality to eliminate any transients associated with the initialization, yielding a clean, single KAW with kρi=1k_{\perp}\rho_{i}=1. The simulation is then restarted with lowered collisionalities νs/(k0vti)=2×103\nu_{s}/(k_{\parallel 0}v_{ti})=2\times 10^{-3} and evolved to allow collisionless wave-particle interactions to damp the wave. We have verified that the collisionless damping rates of the initialized KAWs agree with the analytical predictions from Vlasov-Maxwell and gyrokinetic linear dispersion relations.

3.2 The Velocity-Space Signature of Transit-Time Damping

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(a)                                                   (b)

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(c)                                                   (d)

Figure 3: Analysis of correlation interval selection for βi=1\beta_{i}=1 AstroGK single KAW simulation. Top row: time evolution of (a) the rate of change of ion kinetic energy density due to TTD, denoted as Wi/t\partial W_{i}/\partial t, and (b) the reduced correlation CδB,i(v,t)C_{\delta B_{\parallel,i}}(v_{\parallel},t) at v=1.1vtiv_{\parallel}=1.1v_{ti}. Both quantities are presented over a range of τωA\tau\omega_{A} values from 0 to 10. The selected τωA\tau\omega_{A} value of 5.5 is marked with a black line. Bottom row: timestack plots of the reduced correlation CδB,i(v,t)C_{\delta B_{\parallel,i}}(v_{\parallel},t) for (c) τωA=0\tau\omega_{A}=0 and (d) τωA=5.5\tau\omega_{A}=5.5, with the vertical dashed line at v/vti=1.137v_{\parallel}/v_{\text{ti}}=1.137 labelling the normalized parallel phase velocity ω/(kvti)\omega/(k_{\parallel}v_{\text{ti}}).

We select the βi=1\beta_{i}=1 single KAW simulation as a fiducial case to determine the velocity-space signature of TTD with (7) and compare it to the known velocity-space signature of LD using only the parallel contribution to the dot product in (4) (Klein & Howes, 2016; Howes et al., 2017, 2018; Klein et al., 2017; Chen et al., 2019; Klein et al., 2020; Horvath et al., 2020; Afshari et al., 2021). The linear Vlasov-Maxwell dispersion relation yields a parallel phase velocity normalized to the Alfvén velocity of ω¯ω/(kvA)=1.137\overline{\omega}\equiv\omega/(k_{\parallel}v_{A})=1.137 for a KAW with kρi=1k_{\perp}\rho_{i}=1, βi=1\beta_{i}=1, and Ti/Te=1T_{i}/T_{e}=1, corresponding to a normalized wave period of TωA=5.526T\omega_{A}=5.526.

A key step in the field-particle correlation analysis is to choose an appropriate correlation interval τ\tau over which to time-average the rate of energization to eliminate a possibly larger amplitude signal of oscillatory energy transfer in order to reveal the often smaller secular rate of energy transfer that corresponds to the collisionless damping of the wave (Klein & Howes, 2016; Howes et al., 2017; Klein et al., 2017). In Figure 3, we present a test of different correlation intervals over the range 0τωA100\leq\tau\omega_{A}\leq 10 for the βi=1\beta_{i}=1 single KAW simulation. In panel (a), we plot the velocity-space integrated rate of ion energization due to TTD, (Wi/t)TTD=CδB,i(v,v)d3𝒗(\partial W_{i}/\partial t)_{\mbox{TTD}}=\int C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp})d^{3}\bm{v}, vs. time. The unaveraged correlation (τ=0\tau=0, dark blue) exhibits pronounced oscillations of the net energy transfer vs. time. Setting the correlation interval to one linear wave period τωA=TωA5.5\tau\omega_{A}=T\omega_{A}\simeq 5.5 (black) minimizes the oscillations, providing an optimal choice for τ\tau for a single wave with a well-defined period, as might be expected on theoretical grounds. We show in panel (b) the evolution of the reduced parallel correlation CδB,i(v,t)C_{\delta B_{\parallel},i}(v_{\parallel},t) at a parallel velocity v=1.1vtiv_{\parallel}=1.1v_{\text{ti}} slightly below the resonant velocity. Here again, setting τωA=5.5\tau\omega_{A}=5.5 (black) effectively minimizes the oscillations, revealing clearly the rate of secular energy transfer at that parallel velocity. We illustrate the impact of choosing an appropriate correlation interval τ\tau on the timestack plot of the correlation CδB,i(v,t)C_{\delta B_{\parallel},i}(v_{\parallel},t) by comparing (c) the instantaneous (τ=0\tau=0) field-particle correlation to (d) the correlation using τωA=5.5\tau\omega_{A}=5.5, showing a clear bipolar signature about the normalized parallel phase velocity ω/(kvti)=1.137\omega/(k_{\parallel}v_{ti})=1.137 that persists over the course of the simulation.

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Figure 4: Velocity-space signatures of (a) transit-time damping (TTD) and (b) Landau damping (LD), from the AstroGK simulation of a single kinetic Alfvén wave with kρi=1k_{\perp}\rho_{i}=1, βi=1\beta_{i}=1, and Ti/Te=1T_{i}/T_{e}=1, each showing the gyrotropic signatures in the main panel, the time-integrated reduced parallel signatures in the lower panel, and the net rate of ion energization vs. time for each mechanism in the left panel. The correlation interval is chosen as τωA=5.5\tau\omega_{A}=5.5. The normalized parallel phase velocity is labeled by the two vertical dashed lines at v/vti=±1.137v_{\parallel}/v_{\text{ti}}=\pm 1.137.

Specifying the correlation interval to be approximately one wave period τωA=5.5\tau\omega_{A}=5.5,444Note that the velocity-space signature for a single KAW is independent of the probe position if the correlation interval is taken to be an integral multiple of the wave period. we now present in Figure 4 the velocity-space signatures of (a) TTD and (b) LD from the βi=1\beta_{i}=1 single KAW simulation. Each panel presents three sub-plots, explained here for the TTD case in panel (a): (i) the main plot presents the gyrotropic velocity-space signature CδB,i(v,v)C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp}) at time tωA=63.57t\omega_{A}=63.57, with the parallel phase velocity indicated (vertical dotted line); (ii) the lower plot shows the time-integrated parallel velocity-space signature CδB,i(v)C_{\delta B_{\parallel},i}(v_{\parallel}) to highlight the variation of the net energy transferred as a function of vv_{\parallel}, showing a clear bipolar signature at the parallel phase velocity; and (iii) the left plot shows the velocity-space integrated net energy density transfer rate due to TTD (Wi(t)/t)TTD(\partial W_{i}(t)/\partial t)_{\mbox{TTD}} vs. time, with the centered time of the correlation interval shown in the gyrotropic signature indicated (horizontal solid line). Panel (b) presents the corresponding plots for the LD case.

A key result of this paper is the velocity-space signature of transit time damping plotted on gyrotropic velocity space CδB,i(v,v)C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp}) in Figure 4(a). From the same simulation, the gyrotropic velocity-space signature of LD CE,i(v,v)C_{E_{\parallel},i}(v_{\parallel},v_{\perp}), given by the parallel contribution to the dot-product in (4), is presented in (b) for comparison. The TTD signature agrees qualitatively with our prediction presented in Figure 2(c), showing the key features: (i) the bipolar signature of the rate of loss (blue) and gain (red) of phase-space energy density is centered about the parallel wave phase velocity vω/kv_{\parallel}\sim\omega/k_{\parallel} (vertical dotted black line); (ii) the gyrokinetic velocity-space signature does not extend down to v=0v_{\perp}=0, due to a combination of the v2v_{\perp}^{2} weighting arising from the magnetic moment μ=mv2/(2B)\mu=mv^{2}_{\perp}/(2B) in the mirror force and from the loss cone angle of the mirror force, as explained in §2.2. The LD signature in (b) likewise yields a bipolar signature near the parallel wave phase velocity. Besides the fact that EE_{\parallel} governs energization through LD and EE_{\perp} governs energization through TTD (Howes et al., 2024), a key way to distinguish these two mechanisms is that in gyrotropic velocity space the TTD signature does not extend down to v=0v_{\perp}=0, whereas the LD signature extends right down to v=0v_{\perp}=0.

Careful inspection of these single KAW velocity-space signatures reveals a “twist” seen in both panels of Figure 4, where the bipolar pattern of energy loss (blue) to energy gain (red) across the parallel phase velocity reverses sign as vv_{\perp} changes. This feature arises from the linear combination of three terms contributing to the linear response for perturbed distribution function f1f_{1}, which involves the components of the electric field perturbation and the zeroth-order Bessel function and its derivative, as seen in eq. (4.180) from Swanson (2003). Although a detailed decomposition of these contributions to understand this twist for a single KAW could be performed, for the case of transit-time or Landau damping in a turbulent plasma, this twist is obscured when damping a broadband spectrum of wave modes, as shown in §4, so we do not pursue this line of investigation further.

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(a)                                                   (b)

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(c)                                                   (d)

Figure 5: Velocity-space signatures of transit-time damping (TTD, left column) and Landau damping (LD, right column) in AstroGK single KAW simulations with kρi=1k_{\perp}\rho_{i}=1, Ti/Te=1T_{i}/T_{e}=1, and βi=0.3\beta_{i}=0.3 (top row) and βi=3\beta_{i}=3 (bottom row). The correlation intervals are set to the corresponding linear wave periods, with τωA=5.0\tau\omega_{A}=5.0 for βi=0.3\beta_{i}=0.3 case and τωA=6.2\tau\omega_{A}=6.2 for βi=3\beta_{i}=3 case. The normalized parallel phase velocity is labeled by the two vertical dashed lines at v/vti=±2.313v_{\parallel}/v_{\text{ti}}=\pm 2.313 for βi=0.3\beta_{i}=0.3 and v/vti=±0.583v_{\parallel}/v_{\text{ti}}=\pm 0.583 for βi=3\beta_{i}=3. Each panel follows the layout format of Figure 4.

3.3 Variation of Signature with Ion Plasma Beta βi\beta_{i}

Resonant damping of electromagnetic fluctuations through TTD and LD depends strongly on the plasma beta, typically with LD dominant at βi1\beta_{i}\ll 1 and TTD dominant at βi1\beta_{i}\gg 1 (Quataert, 1998), so we vary the value of βi\beta_{i} here to determine its impact on the characteristics of the velocity-space signature of the Landau-resonant damping mechanisms. Using the same parameters Ti/Te=1T_{i}/T_{e}=1, mi/me=1836m_{i}/m_{e}=1836, and kρi=1k_{\perp}\rho_{i}=1, we perform additional single KAW simulations with βi=0.3\beta_{i}=0.3 and βi=3\beta_{i}=3. For βi=0.3\beta_{i}=0.3, the normalized parallel phase velocity is given by ω¯ω/(kvA)=1.267\overline{\omega}\equiv\omega/(k_{\parallel}v_{A})=1.267 yielding a normalized wave period of TωA=4.959T\omega_{A}=4.959; for βi=3\beta_{i}=3, we obtain ω¯=1.009\overline{\omega}=1.009 and TωA=6.227T\omega_{A}=6.227.

In Figure 5, we plot the velocity-space signatures for (a) TTD and (b) LD for the βi=0.3\beta_{i}=0.3 case and for (c) TTD and (d) LD for the βi=3\beta_{i}=3 case, where each panel has three subplots in the same format as in Figure 4. These bipolar velocity-space signatures look qualitatively similar to the βi=1\beta_{i}=1 case in Figure 4, with two important quantitative differences.

First, the position of the bipolar signature in v/vtiv_{\parallel}/v_{ti} changes as βi\beta_{i} is varied, consistent with the variation of the parallel phase velocity normalized to the ion thermal velocity as βi\beta_{i} varies, given by ω/(kvti)=ω¯/βi1/2\omega/(k_{\parallel}v_{ti})=\overline{\omega}/\beta_{i}^{1/2}. For βi=0.3\beta_{i}=0.3, we obtain ω/(kvti)=2.313\omega/(k_{\parallel}v_{ti})=2.313, indicated by the vertical black dashed line in Figure 5(a) and (b); for βi=3\beta_{i}=3, we obtain ω/(kvti)=0.583\omega/(k_{\parallel}v_{ti})=0.583, as shown in (c) and (d). In both cases, the bipolar signature remains closely associated in vv_{\parallel} with the parallel phase velocity ω/k\omega/k_{\parallel}, as expected for a Landau-resonant energy transfer between the fields and the ions.

Second, looking at the vertical subplots on the left for each panel, which shows the net rate of change of ion energy density WiW_{i} mediated by each mechanism averaged over a correlation interval equal to one wave period τ=T\tau=T, we find the surprising result for βi=0.3\beta_{i}=0.3 that, although LD leads to a net gain of energy by the ions (as expected for collisionless damping of a wave), TTD leads to a net loss of energy from the ions. This finding suggests that the ions are losing energy through the magnetic mirror force while gaining energy through acceleration by the parallel electric field. The rate of ion energy gain by LD is about ten times larger than the rate of loss by TTD, so the summed effect of these two mechanisms is energization of the ions by collisionless damping of the wave, as expected. For the βi=3\beta_{i}=3 case, we find the equally surprising result that although TTD leads to a net gain of energy by the ions, LD is leading to a net loss of energy from the ions; the rate of ion energy gain by TTD is larger than the rate of ion energy loss by LD, so the summed contributions yield a net gain of ion energy as expected for collisionless damping.

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(a)

                  (b)

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Figure 6: Linear dispersion relations for KAWs from PLUME calculations with the realistic mass ratio mi/me=1836m_{i}/m_{e}=1836, showing the absolute value of the normalized wave growth rate |γ|/ω|\gamma|/\omega as a function of the dimensionless perpendicular wave vector kρik_{\perp}\rho_{i} for (a) βi=0.3\beta_{i}=0.3, (b) βi=1\beta_{i}=1, and (c) βi=3\beta_{i}=3. The vertical black dashed line at kρi=1k_{\perp}\rho_{i}=1 indicates the values used in the single KAW AstroGK simulations. We plot γ\gamma (total damping rate, black), γi\gamma_{i} (total ion damping rate, green), γiTTD\gamma_{iTTD} (ion growth or damping rate via the magnetic mirror force, red), and γiLD\gamma_{iLD} (ion growth or damping rate via the electrostatic force, blue). Line styles—solid, dashed, and dotted—represent the total damping rates, damping rates separated by mechanism, and growth rates separated by mechanism, respectively.

How do we reconcile these surprising results with the general expectation of Landau-resonant collisionless damping of waves for a Maxwellian equilibrium velocity distribution? As it turns out, this behavior is exactly what is predicted by the linear Vlasov-Maxwell dispersion relation. To be specific, we take the complex eigenfrequency from the linear dispersion relation to be given by ω+iγ\omega+i\gamma, so that time evolution of a plane-wave mode is given by exp(iωt)exp(γt)\exp(-i\omega t)\exp(\gamma t): positive imaginary components γ>0\gamma>0 correspond to growth of the wave, and negative imaginary components γ<0\gamma<0 correspond to damping of the wave. In Figure 6, we plot the normalized absolute value of the imaginary component of the wave frequency |γ|/ω|\gamma|/\omega vs. kρik_{\perp}\rho_{i} for KAWs using the PLUME solver (Klein & Howes, 2015) for a fully ionized proton-electron plasma with isotropic Maxwellian velocity distributions with Ti/Te=1T_{i}/T_{e}=1, mi/me=1836m_{i}/m_{e}=1836, vti/c=104v_{ti}/c=10^{-4}, kρi=103k_{\parallel}\rho_{i}=10^{-3} over the range 103kρi10210^{-3}\leq k_{\perp}\rho_{i}\leq 10^{2} for the ion plasma beta values (a) βi=0.3\beta_{i}=0.3, (b) βi=1\beta_{i}=1, and (c) βi=3\beta_{i}=3. We plot separately the total collisionless damping rate (black solid) due to both ions and electrons, the total ion damping rate (green solid), and the separate contributions to the ion damping rate from TTD (red) and LD (blue). For the separated TTD and LD contributions, we plot negative imaginary components (which correspond to collisionless damping of the wave) using dashed lines, and positive imaginary components (which correspond to collisionless growth of the wave) using dotted lines.

Although all of the KAW dispersion relations plotted in Figure 6 yield a net effect of collisionless damping by the ions, over some ranges in kρik_{\perp}\rho_{i} (dotted lines) either TTD or LD individually may lead to a net transfer of energy from the ions to the waves over the course of a single wave period. For example, for the βi=3\beta_{i}=3 case in Figure 6(c), the imaginary component due to LD is positive over 1.4×103kρi2.11.4\times 10^{-3}\lesssim k_{\perp}\rho_{i}\lesssim 2.1, corresponding to a transfer of energy from the ions to the wave, and is negative outside of that range, corresponding to a transfer of energy from the wave to the ions. A transfer from ions to the wave would lead to a growth of the wave, but the sum of both of the LD and TTD contributions is always negative for these cases with a Maxwellian velocity distribution, leading to a net collisionless damping of the wave.

The perpendicular wave number kρi=1k_{\perp}\rho_{i}=1 of our simulated single waves is indicated in Figure 6 by the vertical black dashed line, and with these plots we can understand the results presented in Figure 6. For the βi=0.3\beta_{i}=0.3 case, at kρi=1k_{\perp}\rho_{i}=1 we have γiLD<0\gamma_{iLD}<0 (blue dashed) and γiTTD>0\gamma_{iTTD}>0 (red dotted), suggesting that ions gain energy due to EE_{\parallel} but lose energy due to the mirror force when averaged over the full wave period. This finding agrees with the net gain of ion energy by LD in Figure 5(b) and the net loss of ion energy by TTD in (a). Similarly, for the βi=3\beta_{i}=3 case, at kρi=1k_{\perp}\rho_{i}=1 we have γiTTD<0\gamma_{iTTD}<0 (red dashed) and γiLD>0\gamma_{iLD}>0 (blue dotted), suggesting that ions gain energy due to the mirror force but lose energy due to EE_{\parallel} when averaged over the full wave period. Again, this finding from the linear Vlasov-Maxwell dispersion relation agrees with the net gain of ion energy by TTD in Figure 5(c) and the net loss of ion energy by LD in (d).

To further understand the physical meaning of γiTTD>0\gamma_{iTTD}>0 in the βi=0.3\beta_{i}=0.3 case, we first point out that the only mechanism that can change the particle energy is work done by the electric field, and the rate of change of the ion energy density WiW_{i} is given by 𝒋i𝑬\bm{j}_{i}\cdot\bm{E}. For TTD, this energization arises from the component of the electric field that is perpendicular to the magnetic field (Howes et al., 2024) (whereas LD energizes particles through the parallel component of the electric field), so here we consider the perpendicular contribution to the energization jiE{j}_{\perp i}{E}_{\perp}. For a single plane wave, the net transfer of energy to or from the ions by jiE{j}_{\perp i}{E}_{\perp} over a single wave period depends on the phase of the perpendicular electric field fluctuation E{E}_{\perp} relative to the phase of the self-consistent perpendicular component of the ion current density associated with the wave, ji{j}_{\perp i}. If the phase difference δϕ\delta\phi is such that there is an in-phase component 0<δϕ<π/20<\delta\phi<\pi/2, there will be a net energization of the ions; if there is an out-of-phase component π/2<δϕ<π\pi/2<\delta\phi<\pi, the ions will lose energy. The eigenfunctions arising from solutions of the linear Vlasov-Maxwell dispersion relation dictate the phases of the components of the electric field and current density. For the βi=0.3\beta_{i}=0.3 case, this eigenfunction dictates that ji{j}_{\parallel i} and E{E}_{\parallel} are in-phase, leading to ion energization and wave damping by E{E}_{\parallel} (yielding LD), but ji{j}_{\perp i} and E{E}_{\perp} are out-of-phase, so the magnetic mirror force partly counteracts the damping of the wave.

4 Turbulence Simulations

Now that we have determined the gyrotropic velocity-space signature of TTD for single KAWs, with the fiducial example for βi=1\beta_{i}=1 shown in Figure 4(a), we will seek similar signatures of TTD in simulations of strong plasma turbulence.

4.1 Turbulence Simulation Set Up

We perform kinetic simulations of strong plasma turbulence using the Astrophysical Gyrokinetics Code AstroGK (Numata et al., 2010) for three values of the ion plasma beta βi=0.3,1,3\beta_{i}=0.3,1,3. Each simulation has numerical resolution (nx,ny,nz,nλ,nE,ns)=(96,96,32,64,32,2)(n_{x},n_{y},n_{z},n_{\lambda},n_{E},n_{s})=(96,96,32,64,32,2) within a simulation domain L2×L=(8πρi)2×(2πa0)L_{\perp}^{2}\times L_{\parallel}=(8\pi\rho_{i})^{2}\times(2\pi a_{0}), where the elongation of the domain along the equilibrium magnetic field 𝑩0=B0𝒛^\bm{B}_{0}=B_{0}\mbox{$\hat{\bm{z}}$} is characterized by the arbitrary gyrokinetic expansion parameter ϵρi/a01\epsilon\sim\rho_{i}/a_{0}\ll 1. The proton-to-electron temperature ratio of the Maxwellian equilibrium is Ti/Te=1T_{i}/T_{e}=1, and we choose a reduced mass ratio mi/me=36m_{i}/m_{e}=36 to ensure that we fully resolve the kinetic damping mechanisms needed to achieve a steady-state turbulent cascade in a driven simulation, as discussed in Howes et al. (2018). These parameters lead to a fully resolved range of perpendicular wavenumbers 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, or 0.042kρe1.290.042\leq k_{\perp}\rho_{e}\leq 1.29. For the βi=0.3\beta_{i}=0.3 and βi=1\beta_{i}=1 simulations, the proton and electron collisionalities are set to νs/(k0vti)=0.1\nu_{s}/(k_{\parallel 0}v_{ti})=0.1, and for the βi=3\beta_{i}=3 simulation, νs/(k0vti)=0.05\nu_{s}/(k_{\parallel 0}v_{ti})=0.05. These collisionalities ensure weakly collisional plasma conditions, yet prevent the small-scale variations that develop in velocity space from becoming unresolved on the velocity grid.

Turbulence in the simulations is driven from zero initial conditions using an oscillating Langevin antenna (TenBarge et al., 2014) with characteristic frequency ω0/(k0vA)=0.9\omega_{0}/(k_{\parallel 0}v_{A})=0.9 and decorrelation rate σ0/(k0vA)=0.3\sigma_{0}/(k_{\parallel 0}v_{A})=-0.3 to drive four Alfvén wave modes at the domain scale with wave vectors (kxρi,kyρi,kza0)=(0.25,0,±1)(k_{x}\rho_{i},k_{y}\rho_{i},k_{z}a_{0})=(0.25,0,\pm 1) and (0,0.25,±1)(0,0.25,\pm 1), generating four perpendicularly polarized Alfvén waves propagating in both directions along the equilibrium magnetic field. The amplitude of the driving is chosen to satisfy critical balance with a nonlinearity parameter χkδB/(kB0)1\chi\equiv k_{\perp}\delta B_{\perp}/(k_{\parallel}B_{0})\simeq 1 (Goldreich & Sridhar, 1995; Howes et al., 2008a) at the driving scale kρi=0.25k_{\perp}\rho_{i}=0.25. This driving has been shown to generate effectively a strong plasma turbulent cascade to small scales in previous kinetic simulations through nonlinear interactions between the counterpropagating Alfvén waves (Howes et al., 2008b, 2011; Howes & Nielson, 2013; TenBarge & Howes, 2013; TenBarge et al., 2013; Howes et al., 2018; Verniero et al., 2018; Verniero & Howes, 2018; Horvath et al., 2020; Conley et al., 2023). To provide the data needed to apply the field-particle correlation analysis, the electromagnetic fluctuations and proton velocity distributions are sampled at a high cadence at twenty-four probe points that are distributed throughout the domain, sixteen in the xyxy-plane at z=0z=0, and the remaining eight along the zz-axis, as illustrated in Fig. 2 of Horvath et al. (2020).

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Figure 7: Perpendicular magnetic energy spectra at the end of each of the turbulence simulations, showing βi=0.3\beta_{i}=0.3 (red), βi=1\beta_{i}=1 (black), and βi=3\beta_{i}=3 (blue). Vertical dotted lines indicate the limit of fully resolved perpendicular wavenumbers in the simulation, 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, or 0.042kρe1.290.042\leq k_{\perp}\rho_{e}\leq 1.29.

The timescale associated with outer scale of the turbulent cascade in each simulation is the wave period of the domain-scale Alfvén wave TT, and the simulations are run for 6.78T6.78T for the βi=0.3\beta_{i}=0.3 simulation, 5.51T5.51T for the βi=1\beta_{i}=1 simulation, and 3.61T3.61T for the βi=3\beta_{i}=3 simulation. The perpendicular magnetic energy spectrum EB(k)E_{B_{\perp}}(k_{\perp}) at the end of each of the simulations is shown in Figure 7, showing the spectrum for βi=0.3\beta_{i}=0.3 (red), βi=1\beta_{i}=1 (black), and βi=3\beta_{i}=3 (blue). These spectra demonstrate that each simulation yields a broadband turbulent spectrum, with the spectral slope for each simulation consistent with the expectation of 5/3-5/3 for strong plasma turbulence (Goldreich & Sridhar, 1995) in the inertial range at kρi<1k_{\perp}\rho_{i}<1, and steepening of the spectrum at the transition to the dissipation range at kρi1k_{\perp}\rho_{i}\sim 1. In the dissipation range at kρi>1k_{\perp}\rho_{i}>1, the spectral slopes begin around 3.2-3.2, steepening as kρe1k_{\perp}\rho_{e}\rightarrow 1 due to the resolved kinetic dissipation mechanisms that remove energy from the turbulent cascade. Note that these dissipation range slopes are slightly steeper than the values ranging from 2.7-2.7 to 3.1-3.1 typically observed in the solar wind (Sahraoui et al., 2013), but this is to be expected due to the unphysical mass ratio of mi/me=36m_{i}/m_{e}=36, which effectively enhances the damping rate due to electrons relative to the realistic mass ratio case (TenBarge et al., 2013), leading to slightly steeper dissipation range spectra for stronger damping (Howes et al., 2011).

In Figure 8, we plot the normalized damping rates |γ|/ω|\gamma|/\omega from the linear dispersion relation for the simulation parameters with the reduced mass ratio mi/me=36m_{i}/m_{e}=36, presenting the results for (a) βi=0.3\beta_{i}=0.3, (b) βi=1\beta_{i}=1, and (c) βi=3\beta_{i}=3, in the same format as presented in Figure 6. Here we plot vertical black dashed lines at the perpendicular wavenumber limits of the simulation at kρi=0.25k_{\perp}\rho_{i}=0.25 and kρi=7.75k_{\perp}\rho_{i}=7.75. Note the salient features that TTD yields a loss of ion energy for βi=0.3\beta_{i}=0.3 in (a), and LD yields a loss of ion energy for βi=3\beta_{i}=3 at kρi1.5k_{\perp}\rho_{i}\lesssim 1.5. These calculations of the linear wave properties and the effective ion energization rates by TTD and LD provide an important theoretical framework for the interpretation of our field-particle analysis results.

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(a)

                      (b)

                      (c)

Figure 8: Linear dispersion relations for KAWs from PLUME calculations with the reduced mass ratio mi/me=36m_{i}/m_{e}=36, showing the absolute value of the normalized wave damping or growth rate |γ|/ω|\gamma|/\omega as a function of the dimensionless perpendicular wavenumber kρik_{\perp}\rho_{i} for (a) βi=0.3\beta_{i}=0.3, (b) βi=1\beta_{i}=1, and (c) βi=3\beta_{i}=3. The two vertical black dashed lines at kρi=0.25k_{\perp}\rho_{i}=0.25 and 7.757.75 label the range consistent with the AstroGK turbulence simulations, and the two vertical green dashed lines mark the range of 1/e1/e of the peak value of γi\gamma_{i}. The horizontal dashed black line at |γ|/ω=101|\gamma|/\omega=10^{-1} indicates the threshold above which significant damping or growth occurs. Each panel follows the layout format of Figure 6.

4.2 Choosing the Correlation Interval τ\tau

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(a)                                                   (b)

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(c)                                                   (d)

Figure 9: Analysis of correlation interval selection for the βi=1\beta_{i}=1 AstroGK turbulence simulation at Probe 13 (πρi,7πρi,0)(\pi\rho_{i},7\pi\rho_{i},0). Top row: time evolution of (a) the rate of change of ion kinetic energy density due to TTD, denoted as Wi/t\partial W_{i}/\partial t, and (b) the reduced correlation CδB,i(v,t)C_{\delta B_{\parallel,i}}(v_{\parallel},t) at v=1.3vtiv_{\parallel}=-1.3v_{ti}. Both quantities are presented over a range of τωA\tau\omega_{A} values from 0 to 15. The selected τωA\tau\omega_{A} value of 6.4 is marked with a black line. Bottom row: timestack plots of the reduced correlation CδB,i(v,t)C_{\delta B_{\parallel,i}}(v_{\parallel},t) for (c) τωA=0\tau\omega_{A}=0 and (d) τωA=6.4\tau\omega_{A}=6.4, where the range of parallel phase velocities of KAWs that experience significant damping by ions is indicated by vertical dashed lines at v/vti=±1.020v_{\parallel}/v_{\text{ti}}=\pm 1.020 and v/vti=±1.704v_{\parallel}/v_{\text{ti}}=\pm 1.704.

Unlike in the single-KAW simulations, where the single wave period TT is the obvious choice for the correlation interval τ\tau to eliminate the oscillatory contribution to the transfer of energy from fields to particles, choosing τ\tau for a plasma supporting broadband turbulent fluctuations is less straightforward. The longest wave period for an Alfvén wave at the domain scale in our βi=1\beta_{i}=1 simulation is τωA6.28\tau\omega_{A}\simeq 6.28. In Figure 9, for a single probe position in the βi=1\beta_{i}=1 simulation, we present (a) the total energy transfer rate to ions due to TTD (Wi/t)TTD(\partial W_{i}/\partial t)_{\mbox{TTD}} and (b) the energy transfer rate at v/vti=1.3v_{\parallel}/v_{ti}=-1.3, for a correlation interval spanning 0τωA150\leq\tau\omega_{A}\leq 15. The instantaneous values of the local energy transfer rates (with τ=0\tau=0, blue) exhibit large fluctuations with both positive and negative signs, but for τωA=6.4\tau\omega_{A}=6.4 (black) and longer correlation intervals, those large fluctuations are averaged out, leading to a time-averaged energy transfer rate that is about an order-of-magnitude smaller in amplitude than the peaks of the instantaneous value. In Figure 9, we also show timestack plots CδB,i(v,t;τ)C_{\delta B_{\parallel},i}(v_{\parallel},t;\tau) for (c) τ=0\tau=0 and (d) τωA=6.4\tau\omega_{A}=6.4, showing that a relatively persistent bipolar signature of TTD is revealed at v/vti=1.1v_{\parallel}/v_{ti}=-1.1 in the τωA=6.4\tau\omega_{A}=6.4 case with peak amplitudes about an order-of-magnitude smaller than the instantaneous case with τ=0\tau=0. Thus, we choose a correlation interval τωA=6.4\tau\omega_{A}=6.4 to perform the field-particle correlation analysis of our βi=1\beta_{i}=1 turbulence simulation.

4.3 Results for βi=1\beta_{i}=1 Simulation

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(a)                                                            (b)

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(c)                                                            (d)

Figure 10: Velocity-space signatures of transit-time damping (TTD, top row) at Probe 13 (πρi,7πρi,0)(\pi\rho_{i},7\pi\rho_{i},0) and Landau damping (LD, bottom row) at Probe 24 (4πρi,4πρi,0.875πa0)(4\pi\rho_{i},4\pi\rho_{i},0.875\pi a_{0}) in AstroGK turbulence simulation with 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, Ti/Te=1T_{i}/T_{e}=1, and βi=1\beta_{i}=1. The correlation interval is set as τωA=6.4\tau\omega_{A}=6.4. The left column presents gyrotropic plane (v,v)(v_{\parallel},v_{\perp}) signatures, following the layout format of panels in Figure 4. The right column features the timestack plots of the vv_{\perp}-integrated reduced correlation; the main panel here shows the reduced correlation on (v,t)(v_{\parallel},t) grids, and the lower panel shows the time-integrated reduced correlation. Four vertical dashed lines at v/vti=±1.020v_{\parallel}/v_{\text{ti}}=\pm 1.020 and v/vti=±1.704v_{\parallel}/v_{\text{ti}}=\pm 1.704 indicate the resonant parallel phase velocity ranges where significant ion damping occurs.

Performing the field-particle correlation analysis with τωA=6.4\tau\omega_{A}=6.4 for TTD and LD at all 24 probe positions in our βi=1\beta_{i}=1 turbulence simulation, we seek the gyrotropic velocity-space signatures of TTD and LD shown in Figure 4. In Figure 10(a), we plot the gyrotropic velocity-space signature CδB,i(v,v;τ)C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp};\tau) at one of the 24 probes, centered in time at tωA=19.71t\omega_{A}=19.71, showing a clear bipolar signature comparable to that shown in Figure 4(a). The range of resonant parallel phase velocities for the kinetic Alfvén wave mode over which significant ion collisionless damping is expected is indicated by the vertical dashed lines; specifically, these lines mark the resonant velocities of the kinetic Alfvén wave mode at kρi0.5k_{\perp}\rho_{i}\simeq 0.5 and kρi2.3k_{\perp}\rho_{i}\simeq 2.3, the points at which the total ion collisionless damping rate drops to a factor 1/e1/e of its peak value at kρi1.3k_{\perp}\rho_{i}\simeq 1.3, as illustrated by the vertical green dashed lines on the linear dispersion relation plot for mi/me=36m_{i}/m_{e}=36 in Figure 8(b). In the lower panel is shown the reduced parallel velocity-space signature CδB,i(v;τ)C_{\delta B_{\parallel},i}(v_{\parallel};\tau) integrated over vv_{\perp}, yielding a clear bipolar signature with a zero crossing at v/vti1.1v_{\parallel}/v_{ti}\simeq-1.1. Note that the zero crossing of this velocity-space signature falls within the expected range of resonant velocities (vertical dashed lines), as expected theoretically for a resonant collisionless damping mechanism. The left panel shows the net rate of ion energization due to TTD (Wi/t)TTD(\partial W_{i}/\partial t)_{\mbox{TTD}} as a function of time, showing net positive ion energization due to TTD at this position over almost the full duration of the simulation. Thus, Figure 10(a) demonstrates that TTD indeed plays a role in the damping of turbulent fluctuations and consequent energization of the ions, a second key result of this paper.

In Figure 10(b), we show a timestack plot CδB,i(v,t;τ)C_{\delta B_{\parallel},i}(v_{\parallel},t;\tau) of the ion energization by TTD at the same probe position as in (a), showing the persistence in time of the reduced parallel velocity-space signature with the zero crossing at v/vti1.1v_{\parallel}/v_{ti}\simeq-1.1. Note that the zero crossing at v/vti1.1v_{\parallel}/v_{ti}\simeq-1.1 in this timestack plot shifts to slightly lower phase velocities near the end of the simulation at tωA>25t\omega_{A}>25, likely due to damping associated with KAWs that have slightly lower perpendicular wavenumbers kρik_{\perp}\rho_{i}, as can occur in broadband turbulence. There is also a relatively short-lived bipolar signature observed at v/vti1v_{\parallel}/v_{ti}\simeq 1 at times tωA<15t\omega_{A}<15, indicating that TTD is also acting on KAWs propagating the other direction along the magnetic field (Afshari et al., 2021).

We perform the analogous field-particle correlation for LD, showing CE,i(v,v;τ)C_{E_{\parallel},i}(v_{\parallel},v_{\perp};\tau) in Figure 10(c), yielding a bipolar gyrotropic velocity-space signature at v/vti1.2v_{\parallel}/v_{ti}\simeq 1.2 at time tωA=24.3t\omega_{A}=24.3, also within the expected range of resonant parallel phase velocities. This finding of the velocity-space signature of LD confirms previous field-particle correlation analyses showing that ion LD plays a role in the dissipation of plasma turbulence (Klein et al., 2017; Howes et al., 2018; Klein et al., 2020; Cerri et al., 2021). The timestack plot CE,i(v,t;τ)C_{E_{\parallel},i}(v_{\parallel},t;\tau) in Figure 10(d) shows this strong bipolar signature of LD at v/vti1.2v_{\parallel}/v_{ti}\simeq 1.2 persists over 22tωA3022\lesssim t\omega_{A}\lesssim 30. In closing, it is worthwhile noting that, to distinguish the velocity-space signature of TTD from that of LD, it is necessary to examine the signatures in gyrotropic velocity space (v,v)(v_{\parallel},v_{\perp}), showing that ion energization is limited to ions with v/vti1v_{\perp}/v_{ti}\gtrsim 1 for TTD, but that ion energization extends down to v0v_{\perp}\rightarrow 0 for LD, as expected by the physical arguments outlined in §3.2.

4.4 Variations with Ion Plasma Beta βi\beta_{i}

Next, we explore how the velocity-space signatures of TTD and LD in plasma turbulence vary with changing the ion plasma beta βi=vti2/vA2\beta_{i}=v_{ti}^{2}/v_{A}^{2}. Because βi\beta_{i} is a function of the ratio of the ion thermal velocity to the Alfvén velocity, it directly characterizes where the parallel wave phase velocity falls with the ion velocity distribution, making it the most important parameter controlling resonant wave-particle interactions in a weakly collisional plasma. Specifically, ω/(kvti)=ω¯βi1/2\omega/(k_{\parallel}v_{ti})=\overline{\omega}\beta_{i}^{-1/2}, where the parallel phase velocity normalized to the Alfvén velocity ω¯ω/(kvA)\overline{\omega}\equiv\omega/(k_{\parallel}v_{A}) typically has a value ω¯1\overline{\omega}\sim 1 for the perpendicular wavelengths kρi1k_{\perp}\rho_{i}\sim 1 at which the ions strongly interact with the waves. Note that, at the perpendicular scale of the domain k0ρi=0.25k_{\perp 0}\rho_{i}=0.25, the Alfvén wave has the ω¯1\overline{\omega}\simeq 1 for all values of βi\beta_{i}, so we simply choose a correlation interval τωA=6.4\tau\omega_{A}=6.4 for all of the turbulence simulation analysis below.

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(a)                                                   (b)

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(c)                                                   (d)

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(e)                                                   (f)

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(g)                                                   (h)

Figure 11: Velocity-space signatures of transit-time damping (TTD, top two rows) and Landau damping (LD, bottom two rows) sampled from AstroGK turbulence simulation with 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, Ti/Te=1T_{i}/T_{e}=1, and βi=0.3\beta_{i}=0.3. The correlation interval is set as τωA=6.4\tau\omega_{A}=6.4. The left column presents gyrotropic plane (v,v)(v_{\parallel},v_{\perp}) signatures, and the right column features the timestack plots of the vv_{\perp}-integrated reduced correlation; both following the layout format of Figure 10. The resonant parallel phase velocity ranges are marked by the four vertical dashed lines at v/vti=±1.832v_{\parallel}/v_{\text{ti}}=\pm 1.832 and v/vti=±2.373v_{\parallel}/v_{\text{ti}}=\pm 2.373. From top to bottom, data are taken from Probe 7 (5πρi,3πρi,0)(5\pi\rho_{i},3\pi\rho_{i},0), Probe 15 (5πρi,7πρi,0)(5\pi\rho_{i},7\pi\rho_{i},0), Probe 20 (4πρi,4πρi,0.125πa0)(4\pi\rho_{i},4\pi\rho_{i},-0.125\pi a_{0}), and Probe 5 (πρi,3πρi,0)(\pi\rho_{i},3\pi\rho_{i},0), respectively.

We plot some typical velocity-space signatures for TTD and LD for the βi=0.3\beta_{i}=0.3 simulation in Figure 11. Note that, for this value of βi=0.3\beta_{i}=0.3, the contribution of TTD is always to remove energy from the ions, as shown in Figure 8(a), so we expect only negative TTD signatures, similar to that shown in Figure 5(a). Consequently, we expect LD to dominate the removal of energy from the turbulence. Performing the TTD analysis to determine CδB,i(v,v;τ)C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp};\tau), we display a typical gyrotropic velocity-space signature in Figure 11(a) with the associated timestack plot at the same probe in (b), showing two bipolar signatures with a net negative energy transfer rate and zero crossings at v/vti±0.7v_{\parallel}/v_{ti}\simeq\pm 0.7. These look like typical reversed TTD signatures, but the phase velocity is not within the expected range 1.8|v/vti|2.41.8\lesssim|v_{\parallel}/v_{ti}|\lesssim 2.4 for a KAW with βi=0.3\beta_{i}=0.3. Only 3 of the 24 probes showed reversed TTD signatures with phase velocities closer to the expected range, as shown in Figure 11(c) and (d) with a bipolar zero crossing around v/vti1.5v_{\parallel}/v_{ti}\simeq-1.5.

Performing the LD analysis to determine CE,i(v,v;τ)C_{E_{\parallel},i}(v_{\parallel},v_{\perp};\tau) on the same βi=0.3\beta_{i}=0.3 turbulence simulation, we find a similar intriguing result that we commonly find bipolar signatures associated with positive energy transfer to ions, but with zero crossings well below the expected range of 1.8|v/vti|2.41.8\lesssim|v_{\parallel}/v_{ti}|\lesssim 2.4. In Figure 11(e), we see two bipolar signatures at v/vti0.7v_{\parallel}/v_{ti}\simeq-0.7 and v/vti1.2v_{\parallel}/v_{ti}\simeq 1.2. Only 2 of the 24 probes recover LD velocity-space signatures in the expected range, such as that shown in Figure 11(g) and (h).

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(a)                                                            (b)

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(c)                                                            (d)

Figure 12: Velocity-space signatures of transit-time damping (TTD, top row) at Probe 22 (4πρi,4πρi,0.375πa0)(4\pi\rho_{i},4\pi\rho_{i},0.375\pi a_{0}) and Landau damping (LD, bottom row) at Probe 5 (πρi,3πρi,0)(\pi\rho_{i},3\pi\rho_{i},0) sampled from AstroGK turbulence simulation with 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, Ti/Te=1T_{i}/T_{e}=1, and βi=3\beta_{i}=3. The correlation interval is set as τωA=6.4\tau\omega_{A}=6.4. The left column presents gyrotropic plane (v,v)(v_{\parallel},v_{\perp}) signatures, and the right column features the timestack plots of the vv_{\perp}-integrated reduced correlation; both following the layout format of Figure 10. The resonant parallel phase velocity ranges are marked by the four vertical dashed lines at v/vti=±0.583v_{\parallel}/v_{\text{ti}}=\pm 0.583 and v/vti=±0.936v_{\parallel}/v_{\text{ti}}=\pm 0.936.

Turning next to the field-particle correlation analysis of the βi=3\beta_{i}=3 turbulence simulation, the linear dispersion relation plot for KAWs in Figure 8(c) shows that LD removes energy from ions for waves with kρi1.7k_{\perp}\rho_{i}\lesssim 1.7, but TTD positively energizes ions over perpendicular wavenumbers with kρi4k_{\perp}\rho_{i}\lesssim 4. At all probes in the simulation, we find bipolar velocity-space signatures of positive energy transfer by TTD to ions at both positive and negative parallel velocities near the expected range 0.58|v/vti|0.940.58\lesssim|v_{\parallel}/v_{ti}|\lesssim 0.94, with a typical case illustrated in Figure 12, showing (a) the gyrotropic velocity-space signature CδB,i(v,v;τ)C_{\delta B_{\parallel},i}(v_{\parallel},v_{\perp};\tau) and (b) the timestack plot CδB,i(v,t;τ)C_{\delta B_{\parallel},i}(v_{\parallel},t;\tau) indicating that these signatures are persistent in time. On the other hand, analyzing the signatures of LD using (c) the gyrotropic velocity-space signature CE,i(v,v;τ)C_{E_{\parallel},i}(v_{\parallel},v_{\perp};\tau) and (d) the timestack plot CE,i(v,t;τ)C_{E_{\parallel},i}(v_{\parallel},t;\tau), the pattern of energy transfer to ions is widely variable, with ions losing energy more than gaining energy, in agreement with the expectations from the linear dispersion relation. During the majority of the time when clear reversed bipolar patterns are visible for LD, they appear to have zero crossings that are close to the expected range of parallel resonant velocities.

Since the field-particle correlation analysis of our single-wave simulations in §3.3 shows that the velocity-space signatures of TTD and LD appear near the resonant parallel velocities of the waves, as illustrated in Figure 5, it raises the question of why the velocity-space signatures in the βi=0.3\beta_{i}=0.3 simulation in Figure 11 often do not appear in the expected range of resonant velocities. There exist at least two possible explanations for this finding: (i) nonlinear transfer from Alfvén waves to other wave modes, and (ii) nonlinear transit-time damping. Before going into the details of each of these possibilities below, it is worthwhile emphasizing that the field-particle correlation technique determines the total energy transfer to particles over the full velocity distribution, meaning that the net energy transfer within a region of velocity space is effectively weighted by the number of particles within that region of the velocity distribution. To illustrate this point, let us focus on the specific example of Figure 11(a), where the range of resonant parallel phase velocities for the Alfvén mode (vertical black lines) occurs in the range 1.8v/vti2.41.8\lesssim v_{\parallel}/v_{ti}\lesssim 2.4. Even if there exists resonant energy transfer to the particles at these suprathermal parallel velocities, a potentially competing mechanism (such as the two possibilities named above) could dominate the net particle energization if it transfers energy to particles lying within the bulk of the velocity distribution at v/vti1v_{\parallel}/v_{ti}\sim 1, where many more particles can participate in the energy transfer. Thus, the velocity-space signatures arising from the field-particle correlation analysis are generally weighted by the underlying velocity distribution to emphasize energy transfer mechanisms interacting with the main part of the velocity distribution at v/vti1v_{\parallel}/v_{ti}\sim 1.

First, let us analyze how nonlinear energy to other wave modes may explain the velocity-space signatures observed in Figure 11. Due to the predominantly Alfvénic nature of fluctuations in space plasma turbulence (Tu & Marsch, 1995; Schekochihin et al., 2009; Bruno & Carbone, 2013), we focus on the collisional damping rates of Alfvénic fluctuations by TTD and LD in this study. However, the plasma turbulence in our gyrokinetic simulations is broadband and may contain slow magnetosonic fluctuations that arise from nonlinear couplings among the turbulent fluctuations. Although slow magnetosonic waves are not generated by nonlinear couplings among the dominantly Alfvénic fluctuations in the MHD limit at kρi1k_{\perp}\rho_{i}\ll 1 (Schekochihin et al., 2009), at the ion kinetic scales kρi1k_{\perp}\rho_{i}\sim 1 it is possible that energy can be nonlinearly transferred into slow magnetosonic fluctuations. These kinetic slow wave fluctuations555The kinetic slow wave fluctuations specified here are the weakly collisional equivalent of the slow magnetosonic wave in the MHD limit; these are compressible waves distinguished from the kinetic fast magnetosonic wave by the having thermal and magnetic pressure fluctuations acting in opposition as restoring forces for the wave. may have a different parallel phase velocity from the Alfvénic fluctuations and thereby mediate damping of the turbulent energy through either TTD or LD at phase velocities that fall within the bulk of the velocity distribution at v/vti1v_{\parallel}/v_{ti}\sim 1. The second possibility is that nonlinear transit-time damping may occur, whereby the beat mode fluctuations (which are not natural wave modes of the system)—arising from nonlinear interactions between Alfvénic fluctuations with different frequencies and wave vectors—can have an effective phase velocity that falls in the core of the velocity distribution, leading to efficient net energy transfer to the ions via collisionless wave-particle interactions.

In closing this discussion about the velocity-space signatures observed in Figure 11, a final point to emphasize is that the clear bipolar signatures of negative energy transfer from ions by TTD in Figure 11(a) and of positive energy transfer to ions by LD in Figure 11(e) for βi=0.3\beta_{i}=0.3 suggest that some resonant energy transfer mechanism is governing the energization in these simulations; the details of this turbulent damping mechanism, which may include nonlinear couplings to other linear wave modes or nonlinear beat modes as suggested above, are clearly a ripe avenue for exploration in future work.

Refer to caption
Figure 13: Ratio of the change of the ion kinetic energy density due to TTD and LD to the total change of the ion kinetic energy density during the analysis time, both averaged over all 24 probes, plotted against βi\beta_{i}. The error bars represent the standard deviations calculated across all probes.

4.5 Net Turbulent Damping as a Function of Ion Plasma Beta βi\beta_{i}

To estimate the net energy density transfer to or from ions mediated by TTD or LD averaged over the volume of the simulation, we integrate the energy density transfer rate due to each mechanism over the duration of each turbulence simulation (after the energy spectra have reached a statistically steady state) and average over all 24 probes for each simulation. This procedure provides a statistical estimate of the total change in ion energy density by each mechanism, denoted by Wi,TTDW_{i,TTD} and Wi,LDW_{i,LD}. We compute the ratio of these ion energy density changes by each mechanism to the total ion energy density change Wi=Wi,TTD+Wi,LDW_{i}=W_{i,TTD}+W_{i,LD}, and plot Wi,TTD/WiW_{i,TTD}/W_{i} (green) and Wi,LD/WiW_{i,LD}/W_{i} (blue) versus the ion plasma beta βi\beta_{i} in Figure 13. Variability in the energy density changes due to TTD and LD is indicated by error bars on each point, computed using the standard deviation of the time-integrated energy density changes at all 24 probes. The red solid line at 11 presents the sum of Wi,TTD/WiW_{i,TTD}/W_{i} and Wi,LD/WiW_{i,LD}/W_{i}, and the black dashed line at zero highlights whether a mechanism yields a positive net energy density transfer to ions or a negative net energy density transfer from ions.

For βi=0.3\beta_{i}=0.3, the ion energization is dominated by LD, with TTD yielding a small and slightly negative energy transfer. The ion LD and TTD contributions to the damping rate from the linear dispersion relation in Figure 8(a) provide intuition about the relative role of these two collisionless damping mechanisms in a turbulent plasma. Note that the broadband turbulence in the simulation consists of wave modes spanning the range 0.25kρi7.750.25\leq k_{\perp}\rho_{i}\leq 7.75, denoted by the two vertical dashed black lines in Figure 8(a), with a monotonically decreasing magnetic energy spectrum, as shown in Figure 7. The net ion energization by each mechanism expected in a given simulation can be intuitively estimated by an integration over kρik_{\perp}\rho_{i} of the product of the damping rate for that mechanism with the electromagnetic energy at each scale. For βi=0.3\beta_{i}=0.3, Figure 8(a) shows that γiTTD>0\gamma_{iTTD}>0 and γiLD<0\gamma_{iLD}<0 over the full range of perpendicular wavenumbers in the simulation, so the numerical finding of net energy transfer rates in Figure 13 appears to be consistent with the expectation from the linear dispersion relation.

For βi=1\beta_{i}=1, both LD and TTD yield net positive energization of the ions, but LD dominates over TTD once more, as seen in Figure 13. This result is broadly consistent with the linear damping rates from the linear dispersion relation plotted in Figure 8(b), where the LD rate integrated over kρik_{\perp}\rho_{i} would be expected to dominate over the TTD rate, but both mechanisms would be expected to yield net positive ion energization rates.

At βi=3\beta_{i}=3, on the other hand, Figure 13 shows that TTD mediates a net positive energy transfer to the ions, while LD governs a net negative energy transfer with a slightly smaller magnitude than the positive TTD energy transfer. The linear dispersion relation results in Figure 8(c) predict a more complicated behavior than the βi=0.3\beta_{i}=0.3 and βi=1\beta_{i}=1 cases: TTD yields ion energization for all kρi5k_{\perp}\rho_{i}\lesssim 5, but LD leads to ion-to-wave energy transfer for kρi1.5k_{\perp}\rho_{i}\lesssim 1.5 and wave-to-ion energy transfer for kρi1.5k_{\perp}\rho_{i}\gtrsim 1.5. The velocity-space integrated rates of energy transfer by each mechanism at each probe—for example, the vertical left panels of Figure 12(a) and (c)—show variations in time that appear to be consistent with these expectations from linear theory. The TTD rates of ion energy density change are generally positive with moderate amplitudes. On the other hand, the LD rates of ion energy density change are somewhat larger in amplitude but vary with both positive and negative rates, such that the net LD rate averaged over all probes is negative and slightly smaller in amplitude than the net TTD rate. This broader variation is evident in the larger standard deviation of the βi=3\beta_{i}=3 values in Figure 13 relative to the βi=0.3\beta_{i}=0.3 and βi=1\beta_{i}=1 cases.

In conclusion, it is worthwhile emphasizing that the expectations from linear theory of the relative contributions to the energy density transfer rates from each mechanism, including their overall sign, is only expected to hold in statistical sense, averaged over a sufficiently large volume. This is particularly true for plasma parameter values where the expected linear damping rate for a given mechanism changes sign within the range of kρik_{\perp}\rho_{i} where significant damping is expected, such as the case for ion LD in the βi=3\beta_{i}=3 simulation. Based on kinetic numerical simulations of turbulence, the rate of change of energy density for species ss given by 𝒋s𝑬\bm{j}_{s}\cdot\bm{E} is highly variable spatially, with variations that can be much larger than the spatially or temporally averaged net value. An example from a simulation of a strongly nonlinear Alfvén wave collision—the nonlinear interaction between counterpropagating Alfvén waves that is argued to be the fundamental building block of astrophysical plasma turbulence (Howes et al., 2012; Howes & Nielson, 2013; Nielson et al., 2013; Howes et al., 2013; Drake et al., 2013; Howes, 2016; Verniero et al., 2018; Verniero & Howes, 2018)— is seen in Fig. 8 of Howes et al. (2018), where the wave-period averaged energy density transfer rates are found to be an order of magnitude smaller than the instantaneous rates. Furthermore, even for an overall damping rate that energizes the plasma particles at the expense of the turbulent electromagnetic energy, the net energy transfer rate averaged over time at single position may be negative, even when the spatially averaged energy transfer rate is positive, as seen in Fig. 8(d) of Howes et al. (2018).

That the turbulent energy damping rate is highly oscillatory, both in space and time, with a much smaller amplitude net energy damping rate that is generally positive (indicating a damping of turbulence and consequent energization of particles), should not be especially surprising. The nonlinear energy transfer from large to small scales by the turbulence is likewise found to be highly oscillatory, with third-moment calculations of the instantaneous energy transfer rates (Kolmogorov, 1941; Politano & Pouquet, 1998) yielding large values of both signs, with the net averaged value having a much smaller amplitude of positive energy transfer to small scales (Coburn et al., 2014, 2015). Thus, field-particle correlation calculations of the energy density transfer rate at a single point, even averaged over a long duration, may still lead to a result in a turbulent plasma that appears to conflict with the expectation from linear theory. Only with a sufficient large statistical average, here estimated using the average over all 24 probe positions, should we expect the results to be consistent with the general expectations of linear theory—the results in Figure 13 indeed appear to be consistent with the general expectations for the relative contributions of LD and TTD from linear theory.

5 Conclusion

Transit-time damping is a well-known mechanism for the resonant collisionless damping of electromagnetic waves exhibiting variations of the magnetic field magnitude along the mean magnetic field direction, mediated by the magnetic mirror force. This mechanism has been proposed as a possible means for removing energy from the fluctuations in weakly collisional plasma turbulence, but to date there exists little direct evidence clearly showing the damping of turbulence via transit-time damping. Here we employ the recently developed field-particle correlation technique to use measurements of the gradient of the magnetic field magnitude and the ion velocity distribution at a single point to determine a velocity-space signature that can be used to identify definitively that transit-time damping plays a role in the damping of plasma turbulence.

We first derive the particular mathematical form of the field-particle correlation for the rate of energy transfer due to transit-time damping in §2.1, and then we predict the velocity-space signature of the rate of change of phase-space energy density due to transit-time damping using a simple model in §2.2. Next, we perform gyrokinetic simulations of single kinetic Alfvén waves to determine the resulting velocity-space signature of transit-time damping numerically, confirming the qualitative features of our prediction, and presenting the first key result of this study: the gyrotropic velocity-space signature of transit-time damping in Figure 4(a).

We contrast the velocity-space signature of transit-time damping with the known bipolar velocity-space signature of Landau damping, showing the same bipolar pattern of phase-space energy density loss below and gain above the resonant parallel phase velocity, but the transit-time damping signature does not extend down to v0v_{\perp}\rightarrow 0 because it is mediated via the magnetic moment of the charged particle μ=mv2/(2B)\mu=mv_{\perp}^{2}/(2B); thus, signatures of transit-time damping and Landau damping can be distinguished in gyrotropic velocity space by examining the behavior at the resonant parallel phase velocity as v0v_{\perp}\rightarrow 0. Furthermore, we find the unexpected result that transit-time damping can lead to a net loss of ion energy over the period of the wave for βi<1\beta_{i}<1 and Landau damping can lead to a net loss of ion energy over the period of the wave for βi>1\beta_{i}>1. This surprising result is explained, however, by examining the separate contributions of transit-time damping and Landau damping to ion damping from the linear Vlasov-Maxwell dispersion relation: for a single linear kinetic Alfvén wave, the net effect of transit-time damping and Landau damping combined for a plasma with a Maxwellian equilibrium ion velocity distribution always leads to a net damping of the wave and net gain of energy by the ions.

Next, we perform three gyrokinetic simulations of weakly collisional plasma turbulence with three values of βi=0.3,1,3\beta_{i}=0.3,1,3 to seek the velocity-space signature of transit-time damping in the damping of the strong turbulent fluctuations. In the βi=1\beta_{i}=1 turbulence simulation, we indeed find a velocity-space signature of transit-time damping as shown in Figure 10(a), indicating that this mechanism does indeed play a role in the dissipation of kinetic plasma turbulence, along with confirming previously demonstrated signatures of Landau damping with ions in Figure 10(c). This second key result of this paper shows clearly the transit-time damping does serve to damp the fluctuations in weakly collisional plasma turbulence.

The relative strength of transit-time damping and Landau damping is predicted to be a strong function of βi\beta_{i} (Quataert, 1998), so we analyze our βi=0.3\beta_{i}=0.3 and βi=3\beta_{i}=3 simulations to confirm this prediction. For βi=3\beta_{i}=3, we indeed find signatures of transit-time damping in the predicted range of resonant parallel phase velocities in Figure 12(a), but Landau damping signatures vary widely, with both positive and negative energy transfer rates to the ions, and a negative overall average consistent with expectations from the linear dispersion relation in Figure 8(c). For βi=0.3\beta_{i}=0.3, however, we discover puzzling bipolar velocity-space signatures of negative energy transfer but with a zero-crossing well below the parallel phase velocity of kinetic Alfvén waves. This may indicate that energy transfer via transit-time damping is occurring through alternative wave modes, such as kinetic slow magnetosonic fluctuations, or through nonlinear transit-time damping via beat wave modes that are generated by nonlinear interactions among the turbulent fluctuations. These possibilities will be explored in future work.

Determining the time-integrated change of ion kinetic energy density due to transit-time damping and Landau damping as a function of βi\beta_{i} from the three simulations, averaged over all of the probes to obtain a reasonable statistical estimate, we find results in Figure 13 that are generally consistent with the expectations from the linear dispersion relation: (i) at βi=0.3\beta_{i}=0.3, transit-time damping is small and slightly negative, while Landau damping is about an order-of-magnitude larger and positive; (ii) at βi=1\beta_{i}=1, both transit-time damping and Landau damping are positive, but again Landau damping is about an order-of-magnitude larger than transit-time damping; and (iii) at βi=3\beta_{i}=3, transit-time damping is large and positive while Landau damping is somewhat smaller and negative. Note that despite one of the mechanisms possibly leading to a net negative transfer of energy from ions to waves, for a sufficiently large statistical sample it is always the subdominant mechanism that is negative, so the net effect of the sum of both of these n=0n=0 Landau resonant collisionless wave-particle interactions (transit-time damping and Landau damping) averaged over all of the probe positions is a damping of the turbulence for equilibrium Maxwellian velocity distributions.

Acknowledgements

Numerical simulations were performed using the Extreme Science and Engineering Discovery Environment (XSEDE), which is supported by National Science Foundation grant number ACI-1548562, through allocation TG-PHY090084.

Funding

Supported by NASA grants 80NSSC18K0643, 80NSSC18K1217, and 80NSSC18K1371 and NSF grant AGS-1842561.

Declaration of interests

The authors report no conflict of interests.

Appendix A Explicit Form of Landau Damping and Transit-Time Damping Terms in Nonlinear Gyrokinetics

The nonlinear, collisionless gyrokinetic equation (Howes et al., 2006) can be manipulated into a form in which the terms governing Landau damping (LD) and transit-time damping (TTD) are readily apparent. We begin with the nonlinear, collisionless gyrokinetic equation in cgs units, Eq. (25) in Howes et al. (2006),

hst+vhsz+cB0[χ𝑹s,hs]=qsF0sT0sχ𝑹st\frac{\partial h_{s}}{\partial t}+v_{\parallel}\frac{\partial h_{s}}{\partial z}+\frac{c}{B_{0}}\left[\langle\chi\rangle_{\bm{R}_{s}},h_{s}\right]=\frac{q_{s}F_{0s}}{T_{0s}}\frac{\partial\langle\chi\rangle_{\bm{R}_{s}}}{\partial t} (11)

where the nonlinear term is expressed in the Poisson bracket, defined by

[U,V]=𝒛^[U𝑹s×V𝑹s]=UXVYUYVX\left[U,V\right]=\mbox{$\hat{\bm{z}}$}\cdot\left[\frac{\partial U}{\partial\bm{R}_{s}}\times\frac{\partial V}{\partial\bm{R}_{s}}\right]=\frac{\partial U}{\partial X}\frac{\partial V}{\partial Y}-\frac{\partial U}{\partial Y}\frac{\partial V}{\partial X} (12)

where the guiding center coordinates are given by 𝑹s=(X,Y,z)\bm{R}_{s}=(X,Y,z). The gyroaverage of a given quantity at the guiding center position for a particle of species ss is denoted by 𝑹s\langle\ldots\rangle_{\bm{R}_{s}}. The gyrokinetic potential is defined by χ(𝒓,t)=ϕ𝒗𝑨/c\chi(\bm{r},t)=\phi-\bm{v}\cdot\bm{A}/c, where ϕ(𝒓,t)\phi(\bm{r},t) is the scalar electrostatic potential and 𝑨(𝒓,t)\bm{A}(\bm{r},t) is the vector potential. In this formulation, the total velocity distribution function for species ss is separated into fs(𝒓,𝒗,t)=F0s(v)+(qsϕ(𝒓,t)/Ts)F0s(v)+hs(𝑹s,v,v,t)+O(ϵ2)f_{s}(\bm{r},\bm{v},t)=F_{0s}(v)+(-q_{s}\phi(\bm{r},t)/T_{s})F_{0s}(v)+h_{s}(\bm{R}_{s},v_{\parallel},v_{\perp},t)+O(\epsilon^{2}), where F0s(v)F_{0s}(v) is the spatially homogeneous and temporally constant equilibrium Maxwellian velocity distribution and hs(𝑹s,v,v,t)h_{s}(\bm{R}_{s},v_{\parallel},v_{\perp},t) is the perturbed gyrokinetic distribution function at the particle guiding center position 𝑹s\bm{R}_{s} (independent of gyrophase θ\theta in cylindrical velocity space).

We transform from the perturbed gyrokinetic distribution function hsh_{s} to the complementary perturbed gyrokinetic distribution function gsg_{s} (Schekochihin et al., 2009), given by

gs(𝑹s,v,v,t)=hs(𝑹s,v,v,t)qsF0sT0sϕ𝒗𝑨c𝑹s,g_{s}(\bm{R}_{s},v_{\parallel},v_{\perp},t)=h_{s}(\bm{R}_{s},v_{\parallel},v_{\perp},t)-\frac{q_{s}F_{0s}}{T_{0s}}\left\langle\phi-\frac{\bm{v}_{\perp}\cdot\bm{A}_{\perp}}{c}\right\rangle_{\bm{R}_{s}}, (13)

substituting for hsh_{s} everywhere in the nonlinear gyrokinetic equation (11). After some simplification, the equation can be rearranged to obtain

gst+vgsz+cB0[χ𝑹s,gs]=qsF0sT0stvAc𝑹s\displaystyle\frac{\partial g_{s}}{\partial t}+v_{\parallel}\frac{\partial g_{s}}{\partial z}+\frac{c}{B_{0}}\left[\langle\chi\rangle_{\bm{R}_{s}},g_{s}\right]=-\frac{q_{s}F_{0s}}{T_{0s}}\frac{\partial}{\partial t}\left\langle\frac{v_{\parallel}A_{\parallel}}{c}\right\rangle_{\bm{R}_{s}}
\displaystyle- qsF0sT0svzϕ𝒗𝑨c𝑹s+qsF0sT0scB0[vAc𝑹s,ϕ𝒗𝑨c𝑹s]\displaystyle\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\frac{\partial}{\partial z}\left\langle\phi-\frac{\bm{v}_{\perp}\cdot\bm{A}_{\perp}}{c}\right\rangle_{\bm{R}_{s}}+\frac{q_{s}F_{0s}}{T_{0s}}\frac{c}{B_{0}}\left[\left\langle\frac{v_{\parallel}A_{\parallel}}{c}\right\rangle_{\bm{R}_{s}},\left\langle\phi-\frac{\bm{v}_{\perp}\cdot\bm{A}_{\perp}}{c}\right\rangle_{\bm{R}_{s}}\right]

We can rearrange the terms on the right-hand side to obtain a more physically illuminating form,

gst\displaystyle\frac{\partial g_{s}}{\partial t} +\displaystyle+ vgsz+cB0[χ𝑹s,gs]\displaystyle v_{\parallel}\frac{\partial g_{s}}{\partial z}+\frac{c}{B_{0}}\left[\langle\chi\rangle_{\bm{R}_{s}},g_{s}\right]
=\displaystyle= qsF0sT0sv[zϕ𝑹s1cA𝑹st]+qsF0sT0sv1B0[(A𝑹s𝑹s×𝒛^)ϕ𝑹s𝑹s]\displaystyle\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\left[-\frac{\partial}{\partial z}\left\langle\phi\right\rangle_{\bm{R}_{s}}-\frac{1}{c}\frac{\partial\left\langle A_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial t}\right]+\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\frac{1}{B_{0}}\left[\left(\frac{\partial\left\langle A_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\times\mbox{$\hat{\bm{z}}$}\right)\cdot\frac{-\partial\left\langle\phi\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\right]
+\displaystyle+ qsF0sT0svz𝒗𝑨c𝑹s+qsF0sT0sv1B0[(A𝑹s𝑹s×𝒛^)1c𝒗𝑨𝑹s𝑹s]\displaystyle\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\frac{\partial}{\partial z}\left\langle\frac{\bm{v}_{\perp}\cdot\bm{A}_{\perp}}{c}\right\rangle_{\bm{R}_{s}}+\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\frac{1}{B_{0}}\left[\left(\frac{\partial\left\langle A_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\times\mbox{$\hat{\bm{z}}$}\right)\cdot\frac{1}{c}\frac{\partial\left\langle\bm{v}_{\perp}\cdot\bm{A}_{\perp}\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\right]

Using the following relations,

A𝑹s𝑹s×𝒛^=δ𝑩𝑹s,\frac{\partial\left\langle A_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\times\mbox{$\hat{\bm{z}}$}=\left\langle\delta\bm{B}_{\perp}\right\rangle_{\bm{R}_{s}}, (16)
qsc𝒗𝑨𝑹s=12qscv2ΩsδB𝑹s=μsδB𝑹s,\frac{q_{s}}{c}\langle\bm{v}_{\perp}\cdot\bm{A}_{\perp}\rangle_{\bm{R}_{s}}=-\frac{1}{2}\frac{q_{s}}{c}\frac{v_{\perp}^{2}}{\Omega_{s}}\langle\delta B_{\parallel}\rangle_{\bm{R}_{s}}=-\mu_{s}\langle\delta B_{\parallel}\rangle_{\bm{R}_{s}}, (17)
zϕ𝑹s1cA𝑹st=E𝑹s,-\frac{\partial}{\partial z}\left\langle\phi\right\rangle_{\bm{R}_{s}}-\frac{1}{c}\frac{\partial\left\langle A_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial t}=\left\langle E_{\parallel}\right\rangle_{\bm{R}_{s}}, (18)
ϕ𝑹s𝑹s=𝑬𝑹s,\frac{-\partial\left\langle\phi\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}=\left\langle\bm{E}_{\perp}\right\rangle_{\bm{R}_{s}}, (19)

we can simplify the result to obtain

gst\displaystyle\frac{\partial g_{s}}{\partial t} +\displaystyle+ vgsz+cB0[χ𝑹s,gs]\displaystyle v_{\parallel}\frac{\partial g_{s}}{\partial z}+\frac{c}{B_{0}}\left[\langle\chi\rangle_{\bm{R}_{s}},g_{s}\right]
=\displaystyle= qsF0sT0sv(𝒛^+δ𝑩𝑹sB0)𝑬𝑹s+F0sT0sv[μs(𝒛^+δ𝑩𝑹sB0)δB𝑹s𝑹s]\displaystyle\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\left(\mbox{$\hat{\bm{z}}$}+\frac{\left\langle\delta\bm{B}_{\perp}\right\rangle_{\bm{R}_{s}}}{B_{0}}\right)\cdot\left\langle\bm{E}\right\rangle_{\bm{R}_{s}}+\frac{F_{0s}}{T_{0s}}v_{\parallel}\left[-\mu_{s}\left(\mbox{$\hat{\bm{z}}$}+\frac{\left\langle\delta\bm{B}_{\perp}\right\rangle_{\bm{R}_{s}}}{B_{0}}\right)\cdot\frac{\partial\left\langle\delta B_{\parallel}\right\rangle_{\bm{R}_{s}}}{\partial\bm{R}_{s}}\right]

Finally, to put this into a more concise form, we recognize that the direction of the total magnetic field (including the perturbation) to the first order is 𝑩=B0𝒛^+𝜹𝑩𝑹s\bm{B}=B_{0}\mbox{$\hat{\bm{z}}$}+\left\langle\bm{\delta B}_{\perp}\right\rangle_{\bm{R}_{s}}, so we can define the unit vector of the total magnetic field direction as 𝒃^\hat{\bm{b}}

𝒃^=B0𝒛^+𝜹𝑩𝑹sB0.\mbox{$\hat{\bm{b}}$}=\frac{B_{0}\mbox{$\hat{\bm{z}}$}+\left\langle\bm{\delta B}_{\perp}\right\rangle_{\bm{R}_{s}}}{B_{0}}. (21)

With this final simplification, we obtain the final result for the nonlinear gyrokinetic equation,

gst+vgsz+cB0[χ𝑹s,gs]=qsF0sT0sv𝒃^𝑬𝑹sF0sT0svμs𝒃^𝑹sδB𝑹s\frac{\partial g_{s}}{\partial t}+v_{\parallel}\frac{\partial g_{s}}{\partial z}+\frac{c}{B_{0}}\left[\langle\chi\rangle_{\bm{R}_{s}},g_{s}\right]=\frac{q_{s}F_{0s}}{T_{0s}}v_{\parallel}\mbox{$\hat{\bm{b}}$}\cdot\left\langle\bm{E}\right\rangle_{\bm{R}_{s}}-\frac{F_{0s}}{T_{0s}}v_{\parallel}\mu_{s}\mbox{$\hat{\bm{b}}$}\cdot\nabla_{\bm{R}_{s}}\left\langle\delta B_{\parallel}\right\rangle_{\bm{R}_{s}} (22)

This equation has a simple physical interpretation with respect to work done on the distribution functions by the fields: the first term on the right-hand side is the effect of Landau damping by electric field parallel to the total magnetic field; and the second term on the right-hand side is the effect of transit-time damping by the magnetic mirror force due to the gradient of the magnetic field magnitude along the total magnetic field, which to lowest order is just due to the parallel magnetic field perturbations, as shown in (6). Note also that the nonlinear term involves interactions between the electromagnetic fields and the plasma particles, but when integrated over all guiding-center space 𝑹s\bm{R}_{s}, it leads to zero net energy change.

Appendix B Gyrokinetic Form of the Field-Particle Correlation

In gyrokinetics, a form of conserved energy inspired from the definition of entropy is calculated by multiplying the complementary perturbed gyrokinetic distribution function gsg_{s} by T0sgs/F0sT_{0s}g_{s}/F_{0s} and integrating over all velocity and physical space (Howes et al., 2006; Brizard & Hahm, 2007; Schekochihin et al., 2009; Li et al., 2016; Howes et al., 2018). Using a similar approach, we can obtain an energy equation for the gyrokinetic phase-space energy density ws(𝑹s,v,v,t)=Tsgs2/(2F0s)w_{s}(\bm{R}_{s},v_{\parallel},v_{\perp},t)=T_{s}g_{s}^{2}/(2F_{0s}) by multiplying (22) by T0sgs/F0sT_{0s}g_{s}/F_{0s} to obtain

wst+vwsz+T0scB0F0s[χ𝑹s,gs22]=v𝒃^qs𝑬𝑹sgsvμs𝒃^𝑹sδB𝑹sgs\frac{\partial w_{s}}{\partial t}+v_{\parallel}\frac{\partial w_{s}}{\partial z}+\frac{T_{0s}c}{B_{0}F_{0s}}\left[\langle\chi\rangle_{\bm{R}_{s}},\frac{g_{s}^{2}}{2}\right]=v_{\parallel}\mbox{$\hat{\bm{b}}$}\cdot\left\langle q_{s}\bm{E}\right\rangle_{\bm{R}_{s}}g_{s}-v_{\parallel}\mu_{s}\mbox{$\hat{\bm{b}}$}\cdot\nabla_{\bm{R}_{s}}\left\langle\delta B_{\parallel}\right\rangle_{\bm{R}_{s}}g_{s} (23)

In this formulation, the gyrokinetic form of the field-particle correlation for Landau damping would be given by

CE,s(𝑹0,s,v,v,t)=1τtτ/2t+τ/2v𝒃^qs𝑬𝑹sgs𝑑t,C_{E_{\parallel},s}(\bm{R}_{0,s},v_{\parallel},v_{\perp},t)=\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}v_{\parallel}\mbox{$\hat{\bm{b}}$}\cdot\left\langle q_{s}\bm{E}\right\rangle_{\bm{R}_{s}}g_{s}dt^{\prime}, (24)

and for transit-time damping would be given by

CδB,s(𝑹0,s,v,v,t)=1τtτ/2t+τ/2vμs𝒃^𝑹sδB𝑹sgsdt.C_{\delta B_{\parallel},s}(\bm{R}_{0,s},v_{\parallel},v_{\perp},t)=-\frac{1}{\tau}\int^{t+\tau/2}_{t-\tau/2}v_{\parallel}\mu_{s}\mbox{$\hat{\bm{b}}$}\cdot\nabla_{\bm{R}_{s}}\left\langle\delta B_{\parallel}\right\rangle_{\bm{R}_{s}}g_{s}dt^{\prime}. (25)

Note that the energy transfer in the nonlinear case is simply “linear” collisionless damping occurring along the local total magnetic field direction (which is a nonlinear correction from the equilibrium magnetic field direction 𝑩0=B0𝒛^\bm{B}_{0}=B_{0}\mbox{$\hat{\bm{z}}$}). Note also that, in the gyrokinetic approximation, the nonlinear contribution (known as the parallel nonlinearity) to the field-particle interactions is dropped, as it comes in only at higher order. Thus, nonlinear saturation of Landau damping does not occur in gyrokinetics, but the nonlinear correction of “linear” collisionless damping due to the difference in the total magnetic field direction from the equilibrium magnetic field direction is included in nonlinear gyrokinetics.

Mathematically, the correlations derived from the Vlasov-Maxwell equations, (7) for TTD and the parallel contribution to the dot product in (4) for LD, and the correlations derived from the gyrokinetics, (25) for TTD and (24) for LD are related by the integration by parts. Physically, the Vlasov-Maxwell version correlation calculates the change in phase-space energy density at fixed positions in velocity space (Eulerian perspective). In contrast, the gyrokinetic version correlation measures the energy changes experienced by particles along their orbits (Lagrangian perspective) (Montag & Howes, 2022). The gyrokinetic version is effectively the same as the alternative field-particle correlation previously defined (Howes et al., 2017), denoted by the symbol CC^{\prime} instead of CC. Therefore, as illustrated in Figure 14, where we plot both the Vlasov-Maxwell version correlations and the gyrokinetic version correlations for the fiducial single-KAW simulation, the loss and gain of phase-space energy density in the velocity space are visible in the Vlasov-Maxwell version correlation plots with the zero-crossing centered at the resonant velocity. Conversely, the gyrokinetic version correlation plots highlight the pure energization of particles, with the peak positioned at the resonant velocity.

We choose not to use the particular forms of the field-particle correlations in (24) and (25) for the study here because the gyrokinetic formulation is the lowest order contribution to the rate of change of phase-space energy density in the gyrokinetic limit of small fluctuations relative to the equilibrium gs/F0s1g_{s}/F_{0s}\ll 1 (Howes et al., 2006); we prefer to establish a form that is appropriate for fluctuations of arbitrary amplitude, which is given for TTD by the form in (7).

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(a)                                                   (b)

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(c)                                                   (d)

Figure 14: Velocity-space signatures of transit-time damping (top row) and Landau damping (bottom row), plotted from a single kinetic Alfvén wave AstroGK simulation data with kρi=1,βi=1,Ti/Te=1k_{\perp}\rho_{i}=1,\beta_{i}=1,T_{i}/T_{e}=1. The Vlasov-Maxwell Version correlations, (7) for TTD and the parallel component of (4) for LD, are applied in the left column; and the gyrokinetic version correlations, (25) for TTD and (24) for LD, are applied in the right column. The layout format, simulation data, correlation interval, and normalized parallel phase velocity presented in this figure are identical to those used in Figure 4.

Appendix C Separating Landau Damping from Transit-Time Damping

As shown by (22), the nonlinear gyrokinetic equation can be manipulated into a form in which the terms governing Landau damping and transit-time damping are explicitly separated. Here we explain how one can separate the contributions to the damping rate γs\gamma_{s} for a given species ss by Landau damping and transit-time damping, both arising from the n=0n=0 Landau resonance, in the Vlasov-Maxwell linear dispersion relation (Stix, 1992; Swanson, 2003) in the limit γs/ω0\gamma_{s}/\omega\rightarrow 0.

The rate of work done on a species ss by the electric field in a plasma is given by

Ps(𝒓,t)=𝒋s(𝒓,t)𝑬(𝒓,t)P_{s}(\bm{r},t)=\bm{j}_{s}(\bm{r},t)\cdot\bm{E}(\bm{r},t) (26)

where the fields 𝒋s\bm{j}_{s} and 𝑬\bm{E} must be real. For a single plane-wave mode of an arbitrary vector field 𝑨\bm{A}, the Fourier transform is given by

𝑨(𝒓,t)=12[𝑨^(𝒌)ei[𝒌𝒓ω(𝒌)t]eγ(𝒌)t+𝑨^(𝒌)ei[𝒌𝒓ω(𝒌)t]eγ(𝒌)t]\bm{A}(\bm{r},t)=\frac{1}{2}\left[\hat{\bm{A}}(\bm{k})e^{i[\bm{k}\cdot\bm{r}-\omega(\bm{k})t]}e^{\gamma(\bm{k})t}+\hat{\bm{A}}^{*}(\bm{k})e^{-i[\bm{k}\cdot\bm{r}-\omega(\bm{k})t]}e^{\gamma(\bm{k})t}\right] (27)

where 𝑨^(𝒌)\hat{\bm{A}}(\bm{k}) is the complex Fourier coefficient for plane-wave vector 𝒌\bm{k} and the complex mode frequency ωc(𝒌)=ω(𝒌)+iγ(𝒌)\omega_{c}(\bm{k})=\omega(\bm{k})+i\gamma(\bm{k}) is a function of 𝒌\bm{k}. Note that for wave vectors 𝒌[,]\bm{k}\in[-\infty,\infty], the reality condition imposes the constraint 𝑨^(𝒌)=𝑨^(𝒌)\hat{\bm{A}}(\bm{k})=\hat{\bm{A}}^{*}(-\bm{k}).

To determine the average energy transfer rate over one wave period Ps(𝒓)T\langle P_{s}(\bm{r})\rangle_{T}, we compute

Ps(𝒓)T=1ToT𝑑t𝒋s(𝒓,t)𝑬(𝒓,t)\langle P_{s}(\bm{r})\rangle_{T}=\frac{1}{T}\int_{o}^{T}dt^{\prime}\bm{j}_{s}(\bm{r},t^{\prime})\cdot\bm{E}(\bm{r},t^{\prime}) (28)

In the case of weak total666For a fully ionized, single-ion plasma, the total damping or growth rate is the sum of the damping or growth rates due to both species, γ=γi+γe\gamma=\gamma_{i}+\gamma_{e}. damping or growth rate, |γ|/ω1|\gamma|/\omega\ll 1,we can substitute in for 𝒋s(𝒙,t)\bm{j}_{s}(\bm{x},t) and 𝑬(𝒙,t)\bm{E}(\bm{x},t) in terms of the complex Fourier coefficients using (27), which enables us to derive

limγ/ω0Ps(𝒓)T=14[𝒋^s(𝒌)𝑬^(𝒌)+𝒋^s(𝒌)𝑬^(𝒌)]\lim_{\gamma/\omega\rightarrow 0}\langle P_{s}(\bm{r})\rangle_{T}=\frac{1}{4}\left[\hat{\bm{j}}_{s}(\bm{k})\cdot\hat{\bm{E}}^{*}(\bm{k})+\hat{\bm{j}}_{s}^{*}(\bm{k})\cdot\hat{\bm{E}}(\bm{k})\right] (29)

as discussed in Sec. 4-2 and eq. (4-5) in Stix (1992).

To progress further, we need to determine the contribution to the plasma current density due to the n=0n=0 resonant terms. In general, the current density for species ss arising from the linear response to an applied electric field 𝑬^(𝒌)\hat{\bm{E}}(\bm{k}) is given by the linear conductivity tensor 𝝈s(ω,𝒌)\bm{\sigma}_{s}(\omega,\bm{k}),

𝒋^s(𝒌)=𝝈s(ω,𝒌)𝑬^(𝒌)=iω4π𝝌s(ω,𝒌)𝑬^(𝒌)\hat{\bm{j}}_{s}(\bm{k})=\bm{\sigma}_{s}(\omega,\bm{k})\cdot\hat{\bm{E}}(\bm{k})=-\frac{i\omega}{4\pi}\bm{\chi}_{s}(\omega,\bm{k})\cdot\hat{\bm{E}}(\bm{k}) (30)

where the linear conductivity tensor can be expressed in terms of the susceptibility 𝝌s(ω,𝒌)\bm{\chi}_{s}(\omega,\bm{k}) for species ss.

Note that the susceptibility tensor 𝝌s\bm{\chi}_{s} involves a sum over all integers nn (the order of the Bessel functions that arise in the integration over the gyrophase of the particles), as shown clearly in Eq. (10-57) of Stix (1992). The Landau resonance, which gives rise to the collisionless mechanisms of Landau damping and transit-time damping, corresponds to the n=0n=0 term in this sum. Therefore, we need only evaluate the n=0n=0 contribution to 𝝌s\bm{\chi}_{s}, denoted here by 𝝌s(n=0)\bm{\chi}^{(n=0)}_{s}. For an equilibrium magnetic field 𝑩0=B0𝒛^\bm{B}_{0}=B_{0}\mbox{$\hat{\bm{z}}$} and the choice of a wave vector in the (x,z)(x,z) plane, 𝒌=k𝒙^+k𝒛^\bm{k}=k_{\perp}\mbox{$\hat{\bm{x}}$}+k_{\parallel}\mbox{$\hat{\bm{z}}$}, all elements of the rank 2 tensor 𝝌s(n=0)(ω,𝒌)\bm{\chi}^{(n=0)}_{s}(\omega,\bm{k}) involving the index xx are zero, i.e., χxj,s(n=0)=χjx,s(n=0)=0\chi^{(n=0)}_{xj,s}=\chi^{(n=0)}_{jx,s}=0, as shown in Stix Eq. (10-61). Therefore, the n=0n=0 contribution to the current density has 𝒙^𝒋^s(n=0)(𝒌)=0\mbox{$\hat{\bm{x}}$}\cdot\hat{\bm{j}}^{(n=0)}_{s}(\bm{k})=0. Thus, we need only concern ourselves with the work done by E^y\hat{E}_{y} and E^z\hat{E}_{z}.

Physically, Landau damping is governed by the work done by the E^z\hat{E}_{z} component of the wave electric field, and transit-time damping is governed by the work done by the E^y\hat{E}_{y} component of the wave electric field (Howes et al., 2024). Since we know that transit-time damping is mediated by the magnetic mirror force, it depends on the gradient of the magnitude of the magnetic field along the magnetic field direction, 𝒃^|𝑩|\mbox{$\hat{\bm{b}}$}\cdot\nabla|\bm{B}|. In the limit of small amplitudes |δ𝑩|B0|\delta\bm{B}|\ll B_{0} appropriate for linear wave theory with total magnetic field 𝑩=𝑩0+δ𝑩\bm{B}=\bm{B}_{0}+\delta\bm{B}, the variations of the magnitude of the total magnetic field 𝑩=𝑩0+δ𝑩\bm{B}=\bm{B}_{0}+\delta\bm{B} can be expressed as δ|𝑩|δB\delta|\bm{B}|\simeq\delta B_{\parallel}, as shown by (6). Note that, with variations only in the xx and zz directions (due to our chosen wavevector orientation), Faraday’s Law gives

Bzt=cEyx,\frac{\partial B_{z}}{\partial t}=-c\frac{\partial E_{y}}{\partial x}, (31)

where δBz=δB\delta B_{z}=\delta B_{\parallel}. Therefore, the variations of the magnetic field magnitude that cause the mirror force arise from the E^y\hat{E}_{y} component of the electric field.

Since χxj,s(n=0)=χjx,s(n=0)=0\chi^{(n=0)}_{xj,s}=\chi^{(n=0)}_{jx,s}=0, we can write the components j^y,s\hat{j}_{y,s} and j^z,s\hat{j}_{z,s} in terms of the susceptibility tensor acting on E^y\hat{E}_{y} and E^z\hat{E}_{z}.

𝒋^s(n=0)(𝒌)=iω(𝒌)4π(0000χyy,s(n=0)(𝒌)χyz,s(n=0)(𝒌)0χzy,s(n=0)(𝒌)χzz,s(n=0)(𝒌))(0E^y(𝒌)E^z(𝒌))\hat{\bm{j}}^{(n=0)}_{s}(\bm{k})=-\frac{i\omega(\bm{k})}{4\pi}\left(\begin{array}[]{ccc}0&0&0\\ 0&\chi^{(n=0)}_{yy,s}(\bm{k})&\chi^{(n=0)}_{yz,s}(\bm{k})\\ 0&\chi^{(n=0)}_{zy,s}(\bm{k})&\chi^{(n=0)}_{zz,s}(\bm{k})\\ \end{array}\right)\left(\begin{array}[]{c}0\\ \hat{E}_{y}(\bm{k})\\ \hat{E}_{z}(\bm{k})\\ \end{array}\right) (32)

Thus, we find

j^y,s(n=0)(𝒌)=iω(𝒌)4π[χyy,s(n=0)(𝒌)E^y(𝒌)+χyz,s(n=0)(𝒌)E^z(𝒌)]\hat{j}^{(n=0)}_{y,s}(\bm{k})=-\frac{i\omega(\bm{k})}{4\pi}\left[\chi^{(n=0)}_{yy,s}(\bm{k})\hat{E}_{y}(\bm{k})+\chi^{(n=0)}_{yz,s}(\bm{k})\hat{E}_{z}(\bm{k})\right] (33)
j^z,s(n=0)(𝒌)=iω(𝒌)4π[χzy,s(n=0)(𝒌)E^y(𝒌)+χzz,s(n=0)(𝒌)E^z(𝒌)]\hat{j}^{(n=0)}_{z,s}(\bm{k})=-\frac{i\omega(\bm{k})}{4\pi}\left[\chi^{(n=0)}_{zy,s}(\bm{k})\hat{E}_{y}(\bm{k})+\chi^{(n=0)}_{zz,s}(\bm{k})\hat{E}_{z}(\bm{k})\right] (34)

Since transit-time damping is mediated by E^y\hat{E}_{y}, using (28) we can compute its energy transfer rate by

PTTD,s(𝒓)T=14[j^y,s(n=0)E^y+j^y,s(n=0)E^y]\langle P_{TTD,s}(\bm{r})\rangle_{T}=\frac{1}{4}\left[\hat{j}^{(n=0)}_{y,s}\hat{E}_{y}^{*}+\hat{j}^{(n=0)*}_{y,s}\hat{E}_{y}\right] (35)

where we have suppressed the explicit dependence on 𝒌\bm{k} of the Fourier components for notational simplicity. Similarly, the energy transfer rate by Landau damping can be computed by

PLD,s(𝒓)T=14[j^z,s(n=0)E^z+j^z,s(n=0)E^z]\langle P_{LD,s}(\bm{r})\rangle_{T}=\frac{1}{4}\left[\hat{j}^{(n=0)}_{z,s}\hat{E}_{z}^{*}+\hat{j}^{(n=0)*}_{z,s}\hat{E}_{z}\right] (36)

Substituting (33) into (35) and taking the limit γ/ω0\gamma/\omega\rightarrow 0, we obtain the expression for the energy transfer rate due to transit-time damping by species ss,

limγ/ω0PTTD,s(𝒓)T=iω16π[(χyy,s(n=0)χyy,s(n=0))E^yE^y+χyz,s(n=0)E^yE^zχyz,s(n=0)E^yE^z]\lim_{\gamma/\omega\rightarrow 0}\langle P_{TTD,s}(\bm{r})\rangle_{T}=-\frac{i\omega}{16\pi}\left[(\chi^{(n=0)}_{yy,s}-\chi^{(n=0)*}_{yy,s})\hat{E}_{y}\hat{E}_{y}^{*}+\chi^{(n=0)}_{yz,s}\hat{E}_{y}^{*}\hat{E}_{z}-\chi^{(n=0)*}_{yz,s}\hat{E}_{y}\hat{E}_{z}^{*}\right] (37)

Substituting (34) into (36) and taking the limit γ/ω0\gamma/\omega\rightarrow 0, we obtain the expression for the energy transfer rate due to Landau damping by species ss,

limγ/ω0PLD,s(𝒓)T=iω16π[(χzz,s(n=0)χzz,s(n=0))E^zE^z+χzy,s(n=0)E^yE^zχzy,s(n=0)E^yE^z]\lim_{\gamma/\omega\rightarrow 0}\langle P_{LD,s}(\bm{r})\rangle_{T}=-\frac{i\omega}{16\pi}\left[(\chi^{(n=0)}_{zz,s}-\chi^{(n=0)*}_{zz,s})\hat{E}_{z}\hat{E}_{z}^{*}+\chi^{(n=0)}_{zy,s}\hat{E}_{y}\hat{E}_{z}^{*}-\chi^{(n=0)*}_{zy,s}\hat{E}_{y}^{*}\hat{E}_{z}\right] (38)

Poynting’s theorem integrated over the plasma volume can be used to connect the period-averaged rate of work done on a plasma species ss by a given collisionless damping mechanism XX to the linear damping rate by that mechanism, γX,s\gamma_{X,s}. For linear dispersion relation solutions, the total damping rate γ\gamma is a linear combination of the damping rates on each species by each mechanism; if only the n=0n=0 Landau resonant mechanisms contribute to the damping in a single ion species and electron plasma, this linear combination is simply γ=γLD,i+γTTD,i+γLD,e+γTTD,e\gamma=\gamma_{LD,i}+\gamma_{TTD,i}+\gamma_{LD,e}+\gamma_{TTD,e}. Separating the contributions from each mechanism XX and each species ss, Poynting’s theorem therefore yields the connection γX,s=PX,s(𝒙)T/(2WEM)\gamma_{X,s}=\langle P_{X,s}(\bm{x})\rangle_{T}/(2W_{EM}), where WEMW_{EM} is the total electromagnetic energy over the integrated volume.

Note that the Stix (1992) representation of the power absorption by species ss, from his Sec. (11-8), is of the form

PsT=(ω8π)[𝑬^𝝈s(a)𝑬^]\langle P_{s}\rangle_{T}=\left(\frac{\omega}{8\pi}\right)\left[\hat{\bm{E}}^{*}\cdot\bm{\sigma}^{(a)}_{s}\cdot\hat{\bm{E}}\right] (39)

where the anti-Hermitian component of the susceptibility is given by

𝝈s(a)=i2(𝝈s𝝈s)\bm{\sigma}^{(a)}_{s}=-\frac{i}{2}(\bm{\sigma}_{s}-\bm{\sigma}^{\dagger}_{s}) (40)

In the examples in Stix (1992) of separating the Landau damping and transit-time damping contributions (see also Quataert, 1998), he artificially sets E^z=0\hat{E}_{z}=0 to determine the power absorption due to transit-time damping, and sets E^y=0\hat{E}_{y}=0 to determine the power absorption due to Landau damping. Such a choice eliminates all of the contributions from the cross-terms of the susceptibility χyz,s\chi_{yz,s} and χzy,s\chi_{zy,s}. However, these terms are not small in general, so their neglect can lead to an inaccurate estimation of the transit-time damping and Landau damping rates. Furthermore, by writing the power absorption in terms of the anti-Hermitian component of the susceptibility 𝝈s(a)\bm{\sigma}^{(a)}_{s}, the terms due to the cross terms χyz,s\chi_{yz,s} and χzy,s\chi_{zy,s} are exchanged between transit-time damping and Landau damping, so the separation of the two different mechanisms is not correct.

C.1 Numerical Results of Landau Damping and Transit-Time Damping Separation

As a demonstration of the separation of the Landau damping and transit-time damping rates for both ions and electrons, we compute linear Vlasov-Maxwell dispersion relation for the Alfvén wave root using PLUME (Klein & Howes, 2015) for a proton-electron plasma with Maxwellian equilibrium velocity distributions with Ti/Te=1T_{i}/T_{e}=1 and plasma parameters βi=1\beta_{i}=1, vti/c=1×104v_{ti}/c=1\times 10^{-4}, and mi/me=1836m_{i}/m_{e}=1836. In Figure 15, we plot the normalized damping (or growth) rates γ/ω\gamma/\omega—where damping corresponds to γ<0\gamma<0 and growth corresponds to γ>0\gamma>0, for kρi=0.01k_{\parallel}\rho_{i}=0.01 over the range d 0.1kρi1000.1\leq k_{\perp}\rho_{i}\leq 100. For this case of isotropic Maxwellian equilibrium velocity distirbutions, there is not source of energy for instabilities, so we obtain a total damping rate γ/ω<0\gamma/\omega<0 (thin black). In the limit small growth or damping rate limit, |γ|/ω1|\gamma|/\omega\ll 1, we separate the ion and electron contributions to the total damping rate, plotting the ion damping or growth rate γi/ω\gamma_{i}/\omega (thin solid red) and the electron damping or growth rate γe/ω\gamma_{e}/\omega (thin solid blue). Note the breakdown of this separation at kρi30k_{\perp}\rho_{i}\gtrsim 30 when the asymptotic small growth or damping rate limit is violated; the practical limit where the breakdown of this separation by species occurs is |γ|/ω0.5|\gamma|/\omega\gtrsim 0.5, as shown in the figure where sum of the ion and electron damping rates deviates from the total damping rate γ/ω\gamma/\omega (thin black) at kρi30k_{\perp}\rho_{i}\gtrsim 30.

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Figure 15: For a plasma with βi=1\beta_{i}=1, Ti/Te=1T_{i}/T_{e}=1, mi/me=1836m_{i}/m_{e}=1836, vti/c=1×104v_{ti}/c=1\times 10^{-4}, and kρi=0.01k_{\parallel}\rho_{i}=0.01, plot of total normalized damping or growth rate γ/ω\gamma/\omega (thin black), ion damping or growth rate γi/ω\gamma_{i}/\omega (red), and electron damping or growth rate γe/ω\gamma_{e}/\omega (blue). The separate contributions to the ion damping rate are γi,LD/ω<0\gamma_{i,LD}/\omega<0 (red short dashed), γi,TTD/ω<0\gamma_{i,TTD}/\omega<0 (red long dashed), and γi,TTD/ω>0\gamma_{i,TTD}/\omega>0 (red dotted). Similarly, The separate contributions to the electron damping rate are γe,LD/ω<0\gamma_{e,LD}/\omega<0 (blue short dashed), γe,TTD/ω<0\gamma_{e,TTD}/\omega<0 (blue long dashed), and γe,TTD/ω>0\gamma_{e,TTD}/\omega>0 (blue dotted).

Examining the separation of the Landau damping from the transit-time damping rates next, we plot in Figure 15 the ion Landau damping rate γi,LD/ω<0\gamma_{i,LD}/\omega<0 (red short dashed), the ion transit-time damping rate γi,TTD/ω<0\gamma_{i,TTD}/\omega<0 (red long dashed), and the ion transit-time growth rate γi,TTD/ω>0\gamma_{i,TTD}/\omega>0 (red dotted). Similarly, we plot the electron Landau damping rate γe,LD/ω<0\gamma_{e,LD}/\omega<0 (blue short dashed), the electron transit-time damping rate γe,TTD/ω<0\gamma_{e,TTD}/\omega<0 (blue long dashed), and the electron transit-time growth rate γe,TTD/ω>0\gamma_{e,TTD}/\omega>0 (blue dotted). Note that for the ions, the transit-time contribution yields wave growth for kρi3k_{\perp}\rho_{i}\geq 3, and effectively cancels out the contribution from ion Landau damping for kρi5k_{\perp}\rho_{i}\geq 5, so the total ion damping rate plummets. For the electrons, the transit-time contribution is positive yielding growth for kρi1.7k_{\perp}\rho_{i}\lesssim 1.7. For kρi0.7k_{\perp}\rho_{i}\lesssim 0.7, γe,LD2γe,TTD\gamma_{e,LD}\simeq-2\gamma_{e,TTD}, so the total electron damping rate is approximately half of the Landau damping contribution. This plot shows clearly that the contributions from one mechanism (LD or TTD) can actually yield growth for certain parameters (meaning energy transfer from the particles to the fields via that mechanisms), even when the overall effect is damping. One can interpret this perhaps puzzling finding with the relative phase between the electric field and the current associated with a particular mechanism. In some cases—e.g., electron damping at kρi1.7k_{\perp}\rho_{i}\lesssim 1.7—this means that energy is transferred from the EzE_{z} component of the electric field to the electrons by Landau damping, but at the same time energy can be transferred from the electrons to the field via the EyE_{y} component of the electric field by transit-time damping. The net effect is damping, but the total damping (or growth) rate is the summation over the Landau and transit-time contributions (which can have either sign). Note also that, for the selection of parameters in this example, the effect of the cyclotron resonance (n0n\neq 0) on the collisionless damping rate is negligible, so the Landau damping and transit-time damping associated with the Landau (n=0n=0) resonance dominates the total wave damping.

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