This work presents mean force emission theory, which extends the classical theory of bremsstrahlung emission to strongly coupled plasmas. In the high-frequency limit, the theory reduces to solving for the electron trajectory during a binary collision, but where the electron–ion interactions occur through the potential of mean force. In the low-frequency limit, it uses an autocorrelation formalism that captures effects of multiple collisions and strongly correlated motion. The predictions are benchmarked by comparison with first-principles classical molecular dynamics simulations of a fully ionized hydrogen plasma in which all interactions are repulsive. The comparison shows good agreement up to Coulomb coupling strengths of Γ 30. The theory improves upon traditional models by including strong coupling effects and systematically including the effect of multiple collisions. Furthermore, mean force emission theory provides evidence that the Drude correction factor commonly used in quantum calculations of optical quantities may not be adequate at strong coupling.

Bremsstrahlung emission plays an important role in radiation transport in a variety of dense plasmas. These include plasmas in nuclear fusion1–3 and astrophysical objects like white dwarfs,4,5 neutron stars,6 and our sun.7 Even in low-temperature industrial applications, such as EUV lithography, the bremsstrahlung emission process is important in modeling energy loss.8,9 Importantly, many of these systems include strongly coupled plasmas. This paper presents mean force emission theory, which extends the description of classical bremsstrahlung into the strongly coupled regime. It also tests this theory by comparing with classical molecular dynamics (MD) simulations of a model plasma that can be simulated in a first-principles manner.

The coupling strength of a plasma can be characterized by the Γ-parameter, defined as
(1)
where a is the Wigner–Seitz radius, T is the temperature, and Z is the ion charge state. Physically, Γ represents the ratio of the potential energy at the average interparticle spacing to the average particle kinetic energy. Values of Γ 1 and Γ 1 correspond to regimes of weak and strong coupling respectively. This paper uses the electron–ion coupling parameter, where a = ( 3 / 4 π n ) 1 / 3 and n is the total plasma density.

Traditional descriptions of the classical bremsstrahlung spectrum apply in the high-frequency limit, which means they treat only the timescale associated with individual electron–ion collisions. A consequence is that they do not capture the low-frequency limit associated with timescales longer than the Coulomb collision time ( τ e i ). Furthermore, early treatments model electron–ion interactions as occurring through the Coulomb potential,10–12 which leads to a logarithmic divergence of the emission spectrum in the low-frequency limit. Later models explored the impact of screening by cutting off the interaction distance at the Debye length,13 or using a linear-dielectric approach that includes Debye–Hückel screening.14 Accounting for screening resolves the divergence, predicting a constant value for the emission coefficient in the low-frequency limit, but does not capture the physical decrease that is expected as the timescale transitions to the fluid-scale associated with multiple collisions. Some authors have looked at bremsstrahlung in strongly coupled plasmas and included the effects of strong correlations through using effective interaction potentials to model electron–ion collisions. These effective potentials include an ion-sphere potential,15 and a soft-core potential with a Yukawa screening term.16 The high-frequency limit of mean force emission theory presented here also addresses strong coupling through an effective interaction potential, but is based on the potential of mean force, which has a rigorous basis in kinetic theory.17 

The bremsstrahlung process has also been approached from a quantum perspective. The seminal work in this regard is Sommerfeld's calculation of non-relativistic quantum electron scattering off a Coulomb potential.18 Subsequent work has looked at the effects of relativity, screening, and electron degeneracy.19–22 In the quantum formalism, strong coupling has been looked at by applying an effective potential to a Kubo–Greenwood approach.23 Quantum effects are conveniently expressed in terms of a single quantity, the Gaunt factor.24 The quantum and classical approaches also agree in that they give similar results for the Gaunt factor when applied to small-angle Coulomb scattering (see Sec. 3.5 in Ref. 12). More importantly for this paper, whether classical or quantum mechanical, any model must account for multiple collisions to capture the low-frequency regime. A popular correction used in quantum calculations of optical transport quantities is a “Drude” factor that includes an effective collision frequency.23,25–27 Mean force emission theory suggests that the form of the Drude factor does not capture strong correlation effects that occur in the neighborhood of the electron plasma frequency.

The mean force emission model is based on mean force kinetic theory,17 which generalizes how the many-body effect of screening should be treated in kinetic theory at strongly coupled conditions. It shows that binary interactions should be modeled via the potential of mean force, rather than the Coulomb or Debye–Hückel potential.28 This has been shown to successfully extend plasma kinetic theory up to Coulomb coupling strengths of Γ 10.29–32 However, kinetic theory only models timescales longer than the Coulomb collision time (τei). Here, we apply the mean force concept to a broad range of timescales in order to capture the full frequency spectrum of bremsstrahlung emission. At high frequencies, the theory looks similar to traditional models, but where electrons and ions interact via the potential of mean force. Under the molecular chaos approximation, these individual collisions are summed up to calculate the emission coefficient. The bremsstrahlung problem can also be reframed in terms of autocorrelation functions in a manner similar to previous work.16 In the low-frequency limit, the velocity autocorrelation is modeled using a Langevin approximation with a temporally local friction force computed from the mean force kinetic theory. This returns a Drude correction factor that captures the asymptotic low frequency decay of the emission spectrum, but misses an enhanced peak that is observed near the plasma frequency. To capture the enhanced peak, a model for the velocity autocorrelation is developed that includes oscillatory behavior associated with strong correlations that the Drude factor misses.

These predictions are benchmarked using classical MD simulations. MD simulations provide first-principles calculations that are commonly utilized to benchmark theories for a variety of physical processes in strongly coupled plasmas, including but not limited to: diffusion,30,33 temperature relaxation,34 thermal conductivity,31 friction,35 and bremsstrahlung absorption.36–38 However, MD simulations present significant complexities when used to simulate multicomponent plasmas with attractive interactions.39 For one, the use of classical point particles and attractive interactions leads to “Coulomb collapse,” where ions and electrons recombine to form classical bound states.40 Even in a weakly coupled system, close interactions between electrons and ions leads to unphysical amounts of radiation. In order to properly account for attractive interactions one needs to include quantum effects at short distances. In order to benchmark the classical theory against first principles classical MD simulations, this work will consider a fully ionized hydrogen plasma with positively charged electrons and ions. While this is a simplified picture, it still provides important information that is applicable to the broader problem at hand. Accurately capturing the surrounding plasma environment in strongly coupled systems and the effect of multiple collisions are details that are universally present in a theoretical description of bremsstrahlung emission, regardless of whether the problem is approached through repulsive interactions and classical physics.

This paper is organized as follows: Sec. II introduces the MD simulations and calculation of the bremsstrahlung emission coefficient. This section also presents a relation between the bremsstrahlung emission and correlation functions. Section III discusses mean force emission theory. Section IV discusses the successes and limitations of mean force emission theory and compares with relevant traditional models. Section V discusses conclusions based on these results.

Molecular dynamics simulations were run using LAMMPS (Large-scale Atomic/Molecular Massively Parallel Simulator).41 These provided a first-principles calculation of the classical dynamics of a collection of charged particles interacting through the electrostatic Coulomb force. For numerical efficiency, the particle–particle particle–mesh (P3M) method was used.42 In P3M, interparticle forces are calculated directly within a specified distance (rc), while outside of this distance charges are interpolated to a grid and the force on a particle is advanced from the electric field computed at the grid cells. To ensure that the computation remains first-principles, rc was chosen so as to not impact the results. In this regard, it was found that r c = 5 a was sufficient for our purpose.

Simulations were run using a two species plasma consisting of positively charged electrons and ions (Z = 1) at a fixed temperature ( T e = T i = T). Because the charge of each species was the same, the simulations can be characterized in dimensionless units entirely by Γ and the mass ratio m i / m e 1836. Each simulation used a three dimensional box with periodic boundary conditions containing 104 particles. Prior to data gathering, each plasma was equilibrated to a fixed Γ value using a Nose–Hoover thermostat.42 Once the particles settled into their equilibrium spatial and velocity distributions the thermostat was turned off, and the total energy in the simulation was fixed. The time step was chosen to be 10 3 ω p e 1 and the total runtime 10 4 ω p e 1, except for the case of the weakest coupling explored ( Γ = 0.01), where the time step was set to 10 4 ω p e 1 in order to fully resolve all collisions. Here ω p e = n e q 2 / ( m e ϵ 0 ) is the electron plasma frequency.

The dipole emission spectrum was calculated using the well-known formula from classical electromagnetism,12 
(2)
where F j ( t ) is the force on each particle j at time t and W ( ω ) represents the energy emitted per unit frequency per sterradian. Equation (2) assumes emission from a thermal plasma that is isotropic. Information about particle forces at each time step is extracted directly from LAMMPS. Note that if all particles in the system had the same charge to mass ratio (q/m), the sum in Eq. (2) would vanish,
(3)
since the sum of the internal forces on the system is zero. Thus, only multi-component plasmas emit dipole radiation. While this may not be true for higher-order emission (quadropole, etc.), this work is only concerned with non-relativistic bremsstrahlung radiation. Higher-order terms only become significant at relativistic particle velocities.43 

In order to relate the calculation of the emission spectrum from Eq. (2) to the forthcoming theoretical work, one can divide by the total time of the simulation ( T) and the simulation volume (V) to calculate the emission coefficient which defines the power density per unit frequency per sterradian j ( ω ) = W ( ω ) / ( T V ). Since the relation between the total spectrum and the emission coefficient is only dependent on parameters T and V, this paper will henceforth refer to results displaying j ( ω ) as the spectrum and the emission coefficient interchangeably.

It is also possible to express j ( ω ) in dimensionless form using the following substitutions:
such that for Z = 1.
(4)
Here, v T e = 2 k B T / m e is the electron thermal velocity. The terms inside the Fourier transform are equivalent to the equations of motion, which in dimensionless form can be shown to depend only on Γ. Thus, qualitatively, the dimensionless emission coefficient depends only on Γ. In the remainder of this paper, the emission coefficient is given in SI units. For the purpose of translating the MD simulation results to physical units, the total plasma density was set to 1 × 10 28 m–3 and the temperature was chosen to be T = 500 , 50 , 5 , 0.5, and 0.05 eV to correspond to coupling strength values of Γ = 0.01 , 0.1 , 1 , 10 , and 100. However, the formulas that are presented still apply to any combination of density and temperature that correspond to a particular value of Γ, and are equally validated by the MD simulations.

Spectra calculated from the MD simulations are shown in Fig. 1. In order to reduce high-frequency noise and isolate the general trends, a third-degree Savitzky–Golay filter was applied in post-processing the data.44 Qualitative changes are observed as a function of coupling strength. Most notably, the spectrum is nearly constant over a wide frequency range at weak coupling, but becomes much more narrow and peaked near the plasma frequency at strong coupling. These breaks in the spectrum can be understood by considering the timescales associated with close interactions, and the transition to macroscopic fluid dynamics.

FIG. 1.

Emission coefficient for a range of coupling strengths ( Γ = 0.01 , 0.1 , 1 , 10 , 100) obtained from MD simulations using Eq. (2). The vertical line is at the electron plasma frequency (ωpe).

FIG. 1.

Emission coefficient for a range of coupling strengths ( Γ = 0.01 , 0.1 , 1 , 10 , 100) obtained from MD simulations using Eq. (2). The vertical line is at the electron plasma frequency (ωpe).

Close modal
At weak coupling, close interactions occur at a timescale characterized by τ min b min / v T e, where b min = Z q 2 / ( 4 π ϵ o k B T ) is the distance of closest approach. This sets a characteristic maximum frequency, ω max τ min 1, so for Z = 1,
(5)
For Γ = 0.01 and 0.1, this predicts ω max / ω p e 1 × 10 3, and 40, respectively, which compares well with the observed break in the constant spectrum at high frequency from the MD results in Fig. 1. Considering the break in the spectrum at low frequency, this is expected to occur at the transition to the fluid dynamical scale, where individual interactions sum to a net fluid that is not accelerating. Taking the timescale associated with this transition to be the Coulomb collision timescale,45 
(6)
this sets a characteristic minimum frequency, ω min τ e i 1, so for Z = 1,
(7)
where Λ = 1 / ( 3 Γ 3 / 2 ) is the plasma parameter. For Γ = 0.01 and 0.1 this gives a prediction of ω min / ω p e 2 × 10 3 and 3 × 10 2, respectively. It is not possible to compare these predictions with the MD data because the length of the simulations only resolved frequencies larger than approximately 10 2 ω p e.

As the coupling strength increases toward unity, the emission spectrum is observed to become less flat and more peaked near the electron plasma frequency. This may be expected from the timescale arguments of Eqs. (5) and (7), since both ω max and ω min merge toward ωpe as Γ approaches 1 (see Fig. 2). Equations (5) and (7) do not apply for values of Γ 1. Accordingly, Fig. 2 uses the expression ln Λ 0.65 ln ( 1 + 2.15 / ( 3 Γ 3 / 2 ) ) from Ref. 33, which extends the electron–ion collision frequency to Γ 1. This expression and previous work have observed that the electron–ion collision frequency plateaus to a value of approximately 0.2 ω p e for Γ 10 (see Fig. 3 of Ref. 29). This appears to agree with the characteristic value of the low-frequency limit in Fig. 1.

FIG. 2.

Characteristic regions of bremsstrahlung emission in terms of frequency and coupling strength. The curve on the left shows the low frequency cutoff from Eq. (7), while the curve on the right shows the high-frequency cutoff from Eq. (5). The merging of these two frequencies at high Γ leads to a peak in emission around the electron plasma frequency.

FIG. 2.

Characteristic regions of bremsstrahlung emission in terms of frequency and coupling strength. The curve on the left shows the low frequency cutoff from Eq. (7), while the curve on the right shows the high-frequency cutoff from Eq. (5). The merging of these two frequencies at high Γ leads to a peak in emission around the electron plasma frequency.

Close modal

The merging of τ min and τei is a characteristic of strong coupling that can also be visualized by examining the time-dependent forces experienced by particles. Each panel in Fig. 3 shows three components of the force on an individual electron in an MD simulation. For the weakest coupling case ( Γ = 0.1), the collisions appear as distinct, random spikes as the electron experiences a strong force during the close encounter with another charged particle. At strong coupling ( Γ = 1 , 10), collisions are not well separated in time. Strong forces do not appear randomly but are a part of a more correlated electron motion through the plasma. In Sec. II C, it is shown that this correlated motion and its impact on the bremsstrahlung emission coefficient can be captured using autocorrelation functions.

FIG. 3.

Three components of the force on an electron during an MD simulation. At Γ = 0.1, the forces show distinct spikes during collisions that are well separated in time. At Γ = 1 and 10, the forces are not well separated in time and display strongly correlated motion.

FIG. 3.

Three components of the force on an electron during an MD simulation. At Γ = 0.1, the forces show distinct spikes during collisions that are well separated in time. At Γ = 1 and 10, the forces are not well separated in time and display strongly correlated motion.

Close modal
The development of a model for the emission spectrum in the low-frequency limit will be aided by an association between Eq. (2) and an autocorrelation function.16 Here, we develop this approximation and test it using the MD simulation data. First, consider an autocorrelation function of the form
(8)
where T represents the total time and, ideally, the limit T is taken. Taking f ( t ) = j ( q j / m j ) F j ( t ) and applying the Wiener–Khinchin theorem,46,47 which relates the power spectrum of a sufficiently random signal and the resulting autocorrelation, shows
(9)
where F { } denotes the Fourier transform. Note that this relationship is approximate because the Wiener–Khinchin theorem applies only to wide-sense stationary random processes.
Non-relativistic bremsstrahlung emission is also almost exclusively due to the ion forces on electrons. To see this one can expand the sum in Eq. (9) such that
(10)
where ∑e and ∑i give the sum of the electronic and ionic forces respectively. It is a very good approximation to drop the second sum since; for example, with fully ionized protons (Z = 1), the sum over ions will be smaller than the sum over electrons by a factor of the mass ratio m e / m i 5 × 10 4. Now, one can separate the remaining forces on electrons into the contributions from ions and electrons such that
(11)
where Ni and Ne represent the number of ions and electrons in the system and F j , k ( t ) and F j , l ( t ) represent the instantaneous force on electron j due to ion k and electron l, respectively. It is straightforward to show that the force contributions from electrons cancel out j = 1 N e l = 1 l j N e F j , l ( t ) = 0, so
(12)
If we further ignore cross-correlations between different electrons [i.e., terms that go like F e 1 ( 0 ) · F e 2 ( t ) where e1 and e2 denote two different electrons] under the assumption that cross correlations decay faster in time than the autocorrelation, then
(13)
where Ne is the number of electrons. The subscript i denotes the force autocorrelation is meant to be calculated from the ion contributions to the force only. Finally, an approximation for the emission coefficient is obtained by combining Eq. (2) with the definition j ( ω ) = W ( ω ) / ( T V ) and the approximations from Eqs. (9) and (13),
(14)
Here, n e = N e / V now represents the electron density.
The force autocorrelation function in Eq. (14) was calculated from the MD simulations by outputting the forces on each electron at specified time steps. A time series of length 100 ω p e 1 with data output every 10 2 ω p e 1 was used to gather the raw data, except at the weakest coupling ( Γ = 0.01) where the time series was sampled every 10 3 ω p e 1. Then, the force autocorrelation was calculated using
(15)
where t0 represents some initial time and the summation is performed over all 5000 electrons in the simulation. In order to increase accuracy, a total of 103 values of t0 (104 for Γ = 0.01) were used to calculate F e ( t 0 ) · F e ( t ) i. Then, an average was performed over all values of t0 to give the autocorrelation functions in Fig. 4. A consequence of this method of averaging is that the data points at the longest times t have the greatest amount of noise. In order to isolate the ionic contributions to the force, the simulations used to calculate the autocorrelation functions were run with electron–electron interactions turned off. While this approach is less physical than keeping the electron–electron interactions on and just taking the ionic contribution directly, it still demonstrates the principle that these autocorrelation functions capture the overall behavior of the bremsstrahlung emission coefficient. It is not practical to isolate the ionic contributions of the forces with the P3M algorithm.
FIG. 4.

Force (a) and velocity (b) autocorrelations calculated from MD simulations and normalized to their initial value. The MD simulations were run with Electron–electron interactions turned off. Both were obtained using Eq. (15) albeit with F replaced with v for the velocity case. In both situations, increasing Γ leads to oscillations that are signatures of strongly correlated motion.

FIG. 4.

Force (a) and velocity (b) autocorrelations calculated from MD simulations and normalized to their initial value. The MD simulations were run with Electron–electron interactions turned off. Both were obtained using Eq. (15) albeit with F replaced with v for the velocity case. In both situations, increasing Γ leads to oscillations that are signatures of strongly correlated motion.

Close modal
The force autocorrelation function from Eq. (14) can be equivalently recast in terms of the velocity autocorrelation function using the relation
(16)
and thus the Fourier transform
(17)
where the factor of 3 comes from definition Z e i ( t ) = 1 3 v e ( t 0 ) · v e ( t ) i. The calculation of the velocity autocorrelation function from MD replaces F in Eq. (15) with v. As before, the subscript i on Z e i ( t ) is meant to denote that this is the electron velocity autocorrelation function due only to electron–ion interactions. The approximation for the emission coefficient from Eq. (4) can then be recast as
(18)
This is a useful approximation because the velocity autocorrelation function has been well studied and characterized in many strongly correlated plasmas.33,48

The force and velocity autocorrelation functions calculated from MD are shown in Fig. 4 for different values of Γ. The characteristic trends in the weakly coupled cases are monotonically decaying correlation functions, whereas the strongly correlated cases exhibit oscillations near the plasma frequency. These oscillations cause the Fourier transforms in Eqs. (14) and (18), and therefore the emission spectrum, to be peaked near the plasma frequency.

The emission coefficient calculated from the force autocorrelations in Eq. (14) is compared to that computed directly from the general formula of Eq. (2) in Fig. 5. The comparison shows that Eq. (14) matches Eq. (2) at all frequencies. Thus, the correlation function approach gives a description of bremsstrahlung emission in the low and mid frequency ranges that is inaccessible to the typical high-frequency approach. In Secs. III C and III D, it is shown that modeling the velocity autocorrelation analytically allows for simple expressions that capture the bremsstrahlung spectrum in the low and mid frequency ranges.

FIG. 5.

Emission coefficient calculated from MD simulations using Eq. (2) compared to calculations using Eq. (14). The calculations using Eq. (14) ignore electron–electron forces. Good agreement across all frequencies justifies using autocorrelation functions to model bremsstrahlung emission.

FIG. 5.

Emission coefficient calculated from MD simulations using Eq. (2) compared to calculations using Eq. (14). The calculations using Eq. (14) ignore electron–electron forces. Good agreement across all frequencies justifies using autocorrelation functions to model bremsstrahlung emission.

Close modal
Mean force emission theory is an extension of mean force kinetic theory17 to a broader range of timescales. Here, particle trajectories are modeled as a sequence of binary collision events, but where the interactions take place via the potential of mean force, rather than the bare Coulomb potential. Finding the trajectory of an electron during a binary collision requires solving Newton's equation of motion,
(19)
where r = r e r i is the relative position between an electron and an ion during a binary interaction.
A major distinction with other models is that the force on the electron in Eq. (19) is the mean force F ¯ e i = w e i ( r ), which is the force obtained when an electron and ion are held at a fixed relative position r e r i, and all other particles are averaged over in a canonical ensemble at equilibrium. It is the negative gradient of the potential of mean force,17,29,49 which is related to the radial distribution function g e i ( r ) by
(20)
Physically, n g e i ( r ) is the statistically averaged density profile of ions around a central electron at equilibrium. Then, w e i ( r ) represents the potential energy of an electron–ion interaction in the presence of all other particles at equilibrium.
In principle, the potential of mean force can be computed from the electron–ion radial distribution function using any means available to compute g e i ( r ). Several possibilities exist, including MD or experimental data. In order to create a self-consistent model that is efficient to evaluate numerically, we apply the classical Ornstein–Zernike (OZ) equation and the hypernetted-chain (HNC) closure,29,49
(21a)
(21b)
where h ( r ) = g ( r ) 1 is the total correlation function, v ( r ) = q 2 / ( 4 π ϵ o r ) is the bare interaction (Coulomb) potential, and hats represent Fourier transformed quantities. The HNC approximation is well known to be accurate for plasmas if Γ 50; see, for example, Fig. 1 of Ref. 29. It can also be extended to solid densities with simple bridge functions.50 
In the weakly coupled limit, the potential of mean force is the Debye–Hückel potential,51 
(22)
where λD is the Debye length. Figure 6 shows how the potential of mean force merges to the Debye–Hückel potential at weak coupling. Around Γ 1, the potentials begin to differ and at strong coupling, the Debye–Hückel potential deviates significantly from the more general potential of mean force.
FIG. 6.

Absolute value of the normalized potential energy ( w / k B T) of an electron around a central ion. Solid lines represent the potential of mean force [Eq. (20)] while dashed lines represent the Debye–Hückel potential [Eq. (22)]. For Γ = 0.01 and 0.1 the Debye–Hückel potential and potential of mean force are identical. For Γ 1, the potential of mean force gives markedly different results than the Debye–Hückel potential. Oscillations in the potential of mean force represent potential wells between neighboring ions.

FIG. 6.

Absolute value of the normalized potential energy ( w / k B T) of an electron around a central ion. Solid lines represent the potential of mean force [Eq. (20)] while dashed lines represent the Debye–Hückel potential [Eq. (22)]. For Γ = 0.01 and 0.1 the Debye–Hückel potential and potential of mean force are identical. For Γ 1, the potential of mean force gives markedly different results than the Debye–Hückel potential. Oscillations in the potential of mean force represent potential wells between neighboring ions.

Close modal
Using the potential of mean force to model binary collisions has a deeper physical basis in kinetic theory. A kinetic description of a collection of particles is contained in the BBGKY (Bogoliubov–Born–Green–Kirkwood–Yvon) hierarchy, an infinite set of equations that relates the n particle distribution function f ( n ) to the n + 1 particle distribution function f ( n + 1 ). The well-known Boltzmann collision operator is derived by taking the limit f ( 3 ) 0 and finding an expression for two particle distribution function f ( 2 ) that appears in the collision operator of the evolution equation for f ( 1 ).52 The Boltzmann collision operator then allows for the calculation of transport quantities, but leads to an infrared divergence due to the assumption that binary collisions occur through the Coulomb potential. Mean force kinetic theory17 instead derives a collision operator by taking the limit Δ f ( 3 ) 0 where
(23)
is a measure of deviation of the three particle distribution function from its value at equilibrium. Here, f o ( n ) is the reduced n-particle distribution function at equilibrium. This leads to a collision operator where binary particle interactions occur through the potential of mean force. However, kinetic theory only treats the velocity change of particles during binary collisions, and therefore averages over the timescale associated with collisions. Modeling the bremsstrahlung emission coefficient requires an extension of mean force kinetic theory to frequency-dependent transport quantities.

Here, we develop this generalization in steps. For high frequencies ( ω ω p e), the spectrum is calculated by solving for the individual trajectories directly from Eq. (19). These are summed to obtain the total emission spectrum in this limit; see Sec. III B. In the low and mid frequency range ( ω ω p e), the spectrum is calculated by summing many trajectories to evaluate the velocity autocorrelation function. This leads to a direct application of mean force kinetic theory to compute an electron–ion collision rate. Then, the spectrum is computed using Eq. (18); see Secs. III C and III D. A simple comprehensive model is then developed that bridges these limits, providing a mean force emission theory that is valid across all frequencies.

In the high-frequency limit, the bremsstrahlung spectrum can be described by considering the short timescale binary collisions between electrons and ions. For a single electron, Eq. (2) is
(24)
Under the molecular chaos approximation, electron–ion collisions are taken to be statistically independent and the pre-collision velocities and positions of the particles are taken to be uncorrelated. Thus, the bremsstrahlung emission coefficient may be calculated by summing the single particle spectrum in Eq. (24) over all possible binary collisions.

The time-dependent force on an electron, F e ( t ), in Eq. (24) is computed by directly solving for the electron trajectory using Eq. (19). Only two coordinates are needed since the collision takes place on a plane. Due to its large mass, the ion is taken to be fixed at the origin and the electron trajectory is started at some distance (d) considered to be asymptotically far away. Asymptotic in this sense refers to a distance larger than the screening length of the potential. Thus, for a weakly coupled plasma, we use d λ D and in a strongly coupled plasma use d a.

The differential emissivity, η ( ω , v ), from an incident electron with speed, v, is then determined by integration over impact parameter, b,
(25)
where the cross sectional area of the collision volume is bdbd ϕ = 2 π bdb. In a complete treatment, the incoming electron speed, v, represents the magnitude of the relative velocity of the electron–ion pair before the interaction. However, under the assumption of thermal equilibrium ( T e = T i = T), the thermal velocity of electrons v T e = 2 k B T / m e is greater than the ions by a factor of m i / m e. Thus, one can neglect the ion motion and this pre-collision relative velocity becomes simply the pre-collision velocity of the electron. The emission coefficient is then determined by integrating η ( ω , v ) over the electron velocity distribution. To compare with the equilibrium MD results, this distribution is a Maxwellian, f M ( v ), so that the emission spectrum in the high-frequency limit is
(26)
where the velocity distribution is assumed to be isotropic ( d 3 v = 4 π v 2 d v).

Figure 7 illustrates an example of the general workflow for computing the high-frequency emission spectrum in Eq. (24). Equation (19) was solved using a Runge–Kutta integrator to give r e ( t ) and v e ( t ) = d r e / d t during a collision. The force felt by the electron was then calculated from the velocity m e d v e / d t and input into Eq. (24) to give the single particle emission spectrum. Finally, the single particle emission spectrum was integrated over impact parameter, b, to find the differential emissivity, Eq. (25), and over pre-collision speed, v, to find the resulting emission coefficient, Eq. (26).

FIG. 7.

General workflow for calculating the single particle spectrum in Eq. (24). Two different impact parameters (b) are shown. (a) The electron trajectories are solved in the collision plane with the potential of mean force centered at the origin. (b) The force-time history is obtained from the trajectories. (c) The single particle spectrum is obtained via Eq. (24).

FIG. 7.

General workflow for calculating the single particle spectrum in Eq. (24). Two different impact parameters (b) are shown. (a) The electron trajectories are solved in the collision plane with the potential of mean force centered at the origin. (b) The force-time history is obtained from the trajectories. (c) The single particle spectrum is obtained via Eq. (24).

Close modal

Figure 8 shows the results of this calculation in comparison with the MD data. For frequencies ( ω > ω p e) the calculated emission coefficient agrees well with MD simulations up to Γ 30. At very strong coupling (Γ = 100), the results are in fair agreement, but begin to depart from MD. This is expected because the high-frequency solution makes the molecular chaos approximation, which becomes increasingly invalid at strong coupling.17,29 For ω < ω p e, the high-frequency solution predicts a constant j ( ω ) as ω 0 and departs from the results given by the MD simulations. This is expected because the high-frequency solution treats only the electron–ion binary collision timescale. In order to capture the low-frequency limit of the spectrum, one needs to include the timescales associated with multiple collisions.

FIG. 8.

High- and low-frequency limits of mean force emission theory compared to MD results. The low frequency solution comes from Eq. (33). The curves for Γ = 0.01 are multiplied by 3 for clarity.

FIG. 8.

High- and low-frequency limits of mean force emission theory compared to MD results. The low frequency solution comes from Eq. (33). The curves for Γ = 0.01 are multiplied by 3 for clarity.

Close modal
In the low-frequency limit ( ω < ω p e), it is useful to consider the description of bremsstrahlung emission given by the correlation functions described in Sec. II C. In Eq. (18), the emission coefficient is given in terms of the electron velocity autocorrelation function Z e i ( t ). If the correlation strength is not too strong, the long time (low frequency) behavior of Z e i ( t ) can be modeled beginning with the Langevin equation for an electron subject to both a systematic frictional force m e ν e i v e ( t ) due to collisions with ions and a randomly fluctuating force R ( t ),53 
(27)
Multiplying by v e ( 0 ), taking the time-average, and making use of the assumption R ( t ) = 0 give the solution
(28)
Evaluating this requires a model for the electron–ion collision frequency, which is provided by the mean force kinetic theory.
In mean force kinetic theory, the electron–ion collision frequency is29,49
(29)
where m e i = m e m i / ( m e + m i ) m e is the reduced mass, v ¯ e i 3 = ( v T e 2 + v T i 2 ) 3 / 2 v T e 3, and Ξei is the lowest order generalized Coulomb logarithm. It is computed from
(30)
where the scattering cross section is
(31)
and the scattering angle is
(32)
Here, ξ = u / v ¯ e i is a normalized relative speed between the electron and ion, ro is the distance of closest approach computed from smallest root of the denominator of Eq. (32), and σ o = π q e 2 q i 2 / ( ( 4 π ϵ ) 2 m e i 2 v ¯ e i 4 ). This is the standard model for summing a series of binary collisions, as in the Boltzmann equation, except that the interaction potential is the potential of mean force, w e i ( r ).
Using the exponential form of Z e i ( t ), Eq. (18) can be evaluated to give a prediction for the emission coefficient in the low-frequency limit,
(33)
Figure 8 shows this expression agrees well with the low-frequency limit from MD simulations up to Γ 10.

While Eq. (33) agrees with MD at low frequencies, it falls short of the emerging peak around ω ω p e in the emission coefficient at strong coupling. Particularly in the case of strong coupling, it is clear from Fig. 4 that Z e i ( t ) is not exponential and there are distinct oscillations at intermediate timescales. In order to better capture the emission coefficient in the mid frequency range, the model of Z e i ( t ) given by Eq. (28) can be modified to account for correlations on intermediate timescales.

In the mid frequency range ( ω p e ω), oscillations in the velocity autocorrelation function at strong coupling cause the exponential model to fail to predict a peak in the emission coefficient around ωpe that is seen in the MD simulations. In order to capture the oscillations in Z e i ( t ) for Γ = 1 30, we propose the following parameterized form:
(34)
where erf is the error function and the fit parameter f ¯ is determined by the following expression:
(35)
Then the resulting emission coefficient for the low and mid-frequency range can be calculated using Eq. (18) to be
(36)

Figure 9 shows that Eq. (36) can effectively capture the peak for Γ = 1 30. It is important to note that the model for Z e i ( t ) in Eq. (34) is not derived from a Langevin-type equation like the previous exponential model. It is possible to more rigorously derive an approximation of Z e i ( t ) by assuming that the frictional force in Eq. (27) is temporally non-local and depends on the past velocity history of the particle; for example, see Hansen and McDonald.53 Although this formalism provides a more rigorous derivation for Z e i ( t ) at strong coupling, the resulting emission coefficient does not approach a constant for high ω and is not convenient for forming a comprehensive solution with the high-frequency model from Sec. III B. The functional form of the velocity autocorrelation model in Eq. (34) is simply motivated by the increasingly oscillatory behavior in Z e i ( t ) at strong coupling. Section III E presents comprehensive solutions for the emission coefficient that apply across all frequencies.

FIG. 9.

Mid-frequency model from Eq. (36) plotted vs MD simulations. This model better captures the growing peak around ωpe between Γ = 1 30. For clarity, the curves for Γ = 1 , 10 , 20 , and 30 are multiplied by 3 , 0.1 , 0.01 , and 0.001, respectively.

FIG. 9.

Mid-frequency model from Eq. (36) plotted vs MD simulations. This model better captures the growing peak around ωpe between Γ = 1 30. For clarity, the curves for Γ = 1 , 10 , 20 , and 30 are multiplied by 3 , 0.1 , 0.01 , and 0.001, respectively.

Close modal

A comprehensive model can be obtained by combining the high-frequency result from Sec. III B with the low- and mid-frequency models presented in Secs. III C and III D. To do this, it is important to note that the high-frequency limit of Eqs. (33) and (36) is constant; see Figs. 8 and 9. Thus, one can simply multiply a frequency-dependent factor onto the high-frequency solution in order to obtain a solution that is valid across all frequencies.

In the case of Eq. (33), the high-frequency solution is modified as
(37)
to obtain a comprehensive solution. Equation (37) is the common Drude normalization that is often applied in quantum calculations of bremsstrahlung emission.23,25–27 In order to account for the mid-frequency peak that is important for Γ = 1 30, using Eq. (36) provides the following comprehensive solution
(38)
The results of Eqs. (37) and (38) are shown in Fig. 10. The comparison with MD data shows that the mean force emission theory matches first principles calculations well up to Γ 30. The Drude formula from Eq. (37) captures the low-frequency limit, but the mid-frequency extension from Eq. (38) is required to capture the peak near ωpe in the strongly coupled regime.
FIG. 10.

Comprehensive models for the mean force emission theory compared to MD simulations. The solid red lines combine the low- and high-frequency limits using Eq. (37), while the dashed blue lines use Eq. (38). The curves for Γ = 0.01 are multiplied by 3 for clarity.

FIG. 10.

Comprehensive models for the mean force emission theory compared to MD simulations. The solid red lines combine the low- and high-frequency limits using Eq. (37), while the dashed blue lines use Eq. (38). The curves for Γ = 0.01 are multiplied by 3 for clarity.

Close modal
Another quantity that is useful to compare between mean force emission theory and the MD simulations is the power radiated by a plasma for a given value of Γ. Specifically, the radiated power density per sterradian (P) can be calculated by integrating the emission coefficient over all frequencies. Using the normalization
(39)
the normalized power becomes
(40)

Figure 11 shows the normalized power computed from MD simulations data vs the prediction using mean force emission theory. The theory predictions agree well with the simulation data up to Γ 30. Furthermore, the emission coefficient from Eq. (38) leads to better agreement with the MD data than the emission coefficient from Eq. (37). Using Eq. (37) to calculate the power leads to an under prediction in the Γ = 1 30 range where the bremsstrahlung peak appears near ω ω p e. The theory also under-predicts the total radiated power for the Γ = 100 data point, as expected from the emission spectrum. Next, we discuss a comparison of the mean force emission theory and previous models.

FIG. 11.

Normalized power from Eq. (40) vs the coupling strength. The solid black curve uses the emission coefficient given by Eq. (38) for Γ = 1 30 while the dashed blue curve uses the emission coefficient from Eq. (37) for all values of Γ.

FIG. 11.

Normalized power from Eq. (40) vs the coupling strength. The solid black curve uses the emission coefficient given by Eq. (38) for Γ = 1 30 while the dashed blue curve uses the emission coefficient from Eq. (37) for all values of Γ.

Close modal
The classical solution to the bremsstrahlung emission problem for a Coulomb potential is summarized by Landau and Lifshitz,10 Oster,11 and Befeki.12 In this theory, binary collisions are solved by using a Coulomb potential to model the electron trajectory and find F e ( t ). This solution is used in Eqs. (24) and (25) to give the following expression for the differential emissivity,
(41)
Here, Ω = ω b min / v , b min = Z q 2 / 4 π ϵ 0 m e v 2 is the classical distance of closest approach for a particle with initial speed v, and K i Ω ( Ω ) and K i Ω ( Ω ) represent the modified Hankel function of order i Ω and its derivative.
Integration of η ( ω , v ) over the velocity distribution, Eq. (26), can be performed either numerically using Eq. (41), or using a low frequency approximation. In the low-frequency approximation, the Hankel function and its derivative are expanded for Ω 1 and the integral in Eq. (26) is performed to give an analytic result,
(42)
where γ 0.577 is Euler's constant and Ω ¯ is Ω evaluated at v = v T e. The limit of Ω 1 corresponds physically to an expansion for small-angle collisions. In general, ln ( 1 / Ω ¯ ) is sometimes referred to as the “Coulomb logarithm.” This analogy to the logarithmic term appearing in many classical plasma transport expressions can be reasoned by noting that 1 / Ω ¯ b max / b min is just the ratio of maximum to minimum impact parameters where b max = v T e / ω. Notice, however, that this logarithmic dependence on frequency is only applicable under specific assumptions: binary collisions occur through the Coulomb potential (no screening) and large-angle collisions are ignored.

Figure 12 shows both the general numerical solution and the small-angle approximation. At high frequencies, the two solutions disagree. Physically, this is because the small-angle approximation ignores large-angle collisions that correspond to high-frequency radiation. Both solutions also diverge logarithmically as ω 0 while the MD results do not. This low-frequency divergence is a direct result of using the Coulomb potential to model binary collisions. The Coulomb potential is long-range, and thus the electron–ion interaction is not negligible when the particles are infinitely far away from each other.

FIG. 12.

Emission coefficients calculated using traditional models compared to MD at weak coupling. The high-frequency (HF) solutions use Coulomb (solid red) and Debye–Hückel potentials (dashed blue). The small angle approximation for the Coulomb potential (dotted red) is shown using Eq. (42). The linear-dielectric approach of Dawson and Oberman (dashed-dotted black) is plotted in the ω ω p e and ω ω p e limits. The limit ω ω p e is the horizontal line. Note that the ω ω p e limit of the Dawson and Oberman and the small angle approximation are on top of each other.

FIG. 12.

Emission coefficients calculated using traditional models compared to MD at weak coupling. The high-frequency (HF) solutions use Coulomb (solid red) and Debye–Hückel potentials (dashed blue). The small angle approximation for the Coulomb potential (dotted red) is shown using Eq. (42). The linear-dielectric approach of Dawson and Oberman (dashed-dotted black) is plotted in the ω ω p e and ω ω p e limits. The limit ω ω p e is the horizontal line. Note that the ω ω p e limit of the Dawson and Oberman and the small angle approximation are on top of each other.

Close modal

Figure 13 further illustrates this point by showing numerical solutions for j ( ω ) obtained by varying the initial distance between the electron and ion when solving for the electron trajectory under a Coulomb potential, then plugging the resultant F e ( t ) into Eqs. (24)–(26). In the low-frequency limit, the solution obtained using a Coulomb potential depends on the initial position. Using a closer initial position is the same as limiting the electron–ion interaction and resolves the low frequency divergence. Increasing the initial position returns the familiar logarithmic divergence as ω 0. In order to resolve this divergence self-consistently, traditional models have considered screening in binary interactions.

FIG. 13.

Emission coefficient obtained by setting the initial electron distance at λ D , 2 λ D , 5 λ D away from the ion. As this distance increases, the curves converge to the traditional high-frequency Coulomb solution (red). This shows that limiting the interaction distance during a binary collision can give the same effect as screening.

FIG. 13.

Emission coefficient obtained by setting the initial electron distance at λ D , 2 λ D , 5 λ D away from the ion. As this distance increases, the curves converge to the traditional high-frequency Coulomb solution (red). This shows that limiting the interaction distance during a binary collision can give the same effect as screening.

Close modal
Disagreement between traditional models using the Coulomb potential and the MD simulations suggest that even at weak coupling screening influences bremsstrahlung emission. One seminal result that includes the effects of screening is that of Dawson and Oberman,14 which is a linear-dielectric approach. The asymptotic limits of this result are given in Befeki,12 
(43)
where A = 2 / ( e 5 γ / 2 ω ) for ω ω p e and A = 2 / ( e γ ω p e ) for ω ω p e. First, the high-frequency limit is essentially the small-angle approximation given by Eq. (42). It is important to note that the analytic result in Eq. (43) includes an ad hoc cutoff at close distances. This ad hoc cutoff is necessary because the linear-dielectric approach does not properly account for the close collisions that produce high-frequency radiation. In the low-frequency limit, the Dawson and Oberman solution resolves the low-frequency divergence and predicts a constant j ( ω ) as ω 0; see Fig. 12.

Figure 12 also shows j ( ω ) obtained using the high-frequency limit from Eq. (26), but based on the Debye–Hückel potential of Eq. (22). Because the Debye–Hückel potential is the Γ 1 limit of the potential of mean force, it matches the MD calculations well at weak coupling and high frequencies. The Debye–Hückel potential is also short-range and thus does not diverge in the low-frequency limit. While the Debye–Hückel potential accurately captures the plateau in j ( ω ) at weak coupling, at strong coupling the simple screening provided by a Debye–Hückel potential fails to accurately predict the results given by MD; see Fig. 14. Indeed, this is where mean force emission theory provides an accurate description by using the potential of mean force.

FIG. 14.

Emission coefficients calculated using traditional models compared to MD at strong coupling. The high-frequency (HF) solutions use Coulomb (solid red) and Debye–Hückel potentials (dashed blue). The small angle approximation for the Coulomb potential (dotted red) is shown using Eq. (42). The linear-dielectric approach of Dawson and Oberman (dashed-dotted black) is shown in the ω ω p e limit. Note that the ω ω p e limit of the Dawson and Oberman and the small angle approximation are on top of each other. Overall, these traditional models fail to account for strong coupling and deviate significantly from MD simulations.

FIG. 14.

Emission coefficients calculated using traditional models compared to MD at strong coupling. The high-frequency (HF) solutions use Coulomb (solid red) and Debye–Hückel potentials (dashed blue). The small angle approximation for the Coulomb potential (dotted red) is shown using Eq. (42). The linear-dielectric approach of Dawson and Oberman (dashed-dotted black) is shown in the ω ω p e limit. Note that the ω ω p e limit of the Dawson and Oberman and the small angle approximation are on top of each other. Overall, these traditional models fail to account for strong coupling and deviate significantly from MD simulations.

Close modal

It is important to note that these traditional approaches do not account for multiple collisions, and are thus limited to high frequencies. Next, we consider a common traditional approach to incorporating multiple collisions.

One common approach used to capture the low-frequency limit of the bremsstrahlung spectrum comes from quantum calculations of the conductivity and absorption coefficient.23,25–27 In this approach, a Kubo–Greenwood solution is corrected at low frequencies by multiplying the solution by a Drude factor ω 2 / ( ν 2 + ω 2 ) where ν is a collision frequency obtained using the conductivity sum rule. This factor comes from the Drude derivation of conductivity, which models a frequency-dependent transport quantity in the low-frequency limit. In local thermodynamic equilibrium, the emission and absorption coefficients are simply related by the Blackbody spectrum, so we expect this multiple collision correction to impact the emission coefficient as well.

Of course, the Drude factor is the solution provided by Eq. (33), derived from the exponential model of the velocity autocorrelation function. Thus, the mean force emission theory justifies the use of a Drude correction in radiation transport calculations for weakly coupled plasmas. However, in strongly correlated plasmas the Drude approach misses the effects of oscillations in Z e i ( t ) that impact the mid frequency range around ω ω p e. In this way, mean force emission theory provides justification for a more complete correction factor that goes beyond the Drude model and captures important effects around the plasma frequency at strong coupling. Although this work is purely classical, it still provides important insight into techniques used in quantum calculations.

The essence of mean force emission theory is that binary electron–ion interactions occur through the potential of mean force. Here, it has been shown that this concept successfully extends the classical theory of bremsstrahlung emission into the strongly coupled regime, showing agreement with MD simulations across the entire frequency range for Γ 30. In terms of coupling strength, it is primarily limited by its application of the molecular chaos approximation, which assumes particles start from an uncorrelated state as an initial condition of their interaction. This is similar to the range of applicability of the previous mean force kinetic theory applied to transport coefficients,17,29,49 and can be considered a generalization of this to a broader range of timescales. In the high-frequency limit, individual binary collisions are summed to predict the emission coefficient. In the low-frequency limit, the theory is recast using autocorrelation functions to capture the effect of multiple successive collisions and this is used to find analytic expressions for the bremsstrahlung emission coefficient. Importantly, the autocorrelation approach shows that in the mid frequency range ( ω ω p e) a peak in emission occurs at strong coupling. This work provides analytic correction factors for the low and mid frequency range that are combined with the high-frequency model to produce a model that applies to all frequencies.

In addition to the intrinsic utility of developing a new theory, this work also gives insight into the physics of common approaches to bremsstrahlung emission in the literature. It emphasizes the importance of screening, even in weakly coupled plasmas, as screening keeps the emission coefficient in traditional models from diverging as ω 0. It also justifies the use of a Drude correction factor in weakly coupled plasmas in order to account for multiple collisions. However, it also suggests that this simple correction may not be enough in strongly coupled plasmas, because strongly correlated motion leads to a peak in emission around the plasma frequency that is not captured by the Drude formula.

Finally, the work here considers a fully ionized hydrogen plasma with positively charged electrons and ions. The inclusion of attractive interactions between electrons and ions is expected to influence the emission coefficient and will be the subject of future work. For one, the electronic trajectories under a repulsive and attractive potential will be different and lead to differences in the high-frequency solution. In the low-frequency limit, the electron–ion collision frequency calculated using mean force kinetic theory is expected to differ between the attractive and repulsive cases. This is known as the Barkas Effect and has been studied rigorously through molecular dynamics simulations and theory.54 However, while the work here considers a simplified model with a repulsively interacting electron–ion plasmas, this development of mean force emission theory lays the groundwork for future calculations that incorporate attractive collisions and quantum effects at short distances.

The authors thank Dr. Charles Starrett for helpful conversations on this work. This work was funded by the NNSA Stockpile Stewardship Academic Alliances under Grant No. DE-NA0004100. Additionally, this research was supported in part through computational resources and services provided by Advanced Research Computing (ARC), a division of Information and Technology Services (ITS) at the University of Michigan, Ann Arbor.

The authors have no conflicts to disclose.

J. P. Kinney: Data curation (lead); Formal analysis (lead); Investigation (lead); Methodology (lead); Visualization (lead); Writing – original draft (lead); Writing – review & editing (equal). H. J. Lefevre: Conceptualization (equal); Funding acquisition (equal); Writing – review & editing (equal). C. C. Kuranz: Conceptualization (equal); Funding acquisition (lead); Writing – review & editing (equal). S. D. Baalrud: Conceptualization (equal); Formal analysis (equal); Funding acquisition (equal); Methodology (equal); Supervision (equal); Writing – review & editing (equal).

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

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