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Chapter 2 • Theory & Derivations

Single-Particle Motion in Uniform Fields & Electric Drifts

Rigorous kinematics and dynamics of charged particles in uniform electromagnetic fields: Lorentz force equation of motion, cyclotron frequency and Larmor radius, helicity and direction of gyration for electrons versus ions, complete mathematical decomposition into guiding center motion and circular gyration, cross-field electric drift velocity derivation and proof of charge/mass independence, general external force drifts (gravitational, centrifugal, collisional drag), time-varying electric fields and the polarization drift velocity, polarization current density, and the low-frequency effective dielectric permittivity of a magnetized plasma.

§2.1 The Fundamental Lorentz Equation of Motion & Gyration in Static Uniform Magnetic Fields

1. The Lorentz Equation of Motion

The classical trajectory of a point particle of rest mass $m$ and electric charge $q$ moving with velocity $\vec{v}$ in macroscopic electric $\vec{E}$ and magnetic $\vec{B}$ fields is governed by Newton's second law with the Lorentz force:

$$m \frac{d\vec{v}}{dt} = q\left( \vec{E} + \vec{v}\times\vec{B} \right)$$

Taking the scalar dot product with the velocity $\vec{v}$:

$$m \vec{v}\cdot\frac{d\vec{v}}{dt} = \frac{d}{dt}\left( \frac{1}{2}m v^2 \right) = q \vec{v}\cdot\vec{E} + q \vec{v}\cdot(\vec{v}\times\vec{B}) = q \vec{v}\cdot\vec{E}$$

Because $\vec{v}\cdot(\vec{v}\times\vec{B}) \equiv 0$, a pure magnetic field does zero work on a charged particle; it alters only the direction of the velocity vector while conserving total kinetic energy $\frac{1}{2}m v^2 = \text{const}$.

2. Gyration in a Static Uniform Magnetic Field

Let $\vec{B} = B_0 \hat{z}$ be static and spatially uniform, with $\vec{E} = 0$. Resolving the equation of motion into Cartesian components:

$$m \frac{dv_x}{dt} = q B_0 v_y, \quad m \frac{dv_y}{dt} = -q B_0 v_x, \quad m \frac{dv_z}{dt} = 0$$

Along the magnetic field, the parallel velocity is constant:

$$v_z(t) = v_\parallel = \text{const} \implies z(t) = z_0 + v_\parallel t$$

Differentiating the $x$-component and substituting $dv_y/dt$:

$$\frac{d^2 v_x}{dt^2} = \frac{q B_0}{m} \frac{dv_y}{dt} = \frac{q B_0}{m} \left( -\frac{q B_0}{m} v_x \right) = -\left( \frac{q B_0}{m} \right)^2 v_x$$

Defining the cyclotron frequency (or gyrofrequency) $\omega_c$:

$$\omega_c \equiv \frac{|q| B_0}{m}$$

The transverse velocity components oscillate harmonically at $\omega_c$:

$$\frac{d^2 v_x}{dt^2} + \omega_c^2 v_x = 0, \quad \frac{d^2 v_y}{dt^2} + \omega_c^2 v_y = 0$$

§2.2 Helical Trajectories, Larmor Radius & Sense of Gyration for Electrons and Ions

1. Larmor Radius & Gyration Circle

Choosing initial conditions such that $v_x(0) = v_\perp \cos\delta$ and integrating:

$$v_x(t) = v_\perp \cos(\mp \omega_c t + \delta), \quad v_y(t) = \pm v_\perp \sin(\mp \omega_c t + \delta)$$

where the upper sign corresponds to positive ions ($q > 0$) and the lower sign to electrons ($q = -e < 0$). Integrating the velocity components yields the spatial coordinates:

$$x(t) = X_0 + \frac{v_\perp}{\omega_c} \sin(\mp \omega_c t + \delta) = X_0 + r_L \sin(\mp \omega_c t + \delta)$$ $$y(t) = Y_0 \mp \frac{v_\perp}{\omega_c} \cos(\mp \omega_c t + \delta) = Y_0 \mp r_L \cos(\mp \omega_c t + \delta)$$

where $(X_0, Y_0)$ represents the fixed center of gyration, known as the guiding center. The radius of the gyration circle is the Larmor radius (or gyroradius) $r_L$:

$$r_L \equiv \frac{v_\perp}{\omega_c} = \frac{m v_\perp}{|q| B_0}$$

2. Helicity and Sense of Gyration

Looking along the direction of $\vec{B}$ (the $+z$ axis):

  • Positive Ions ($q > 0$): Gyrate in a counter-clockwise sense (left-handed rotation).
  • Electrons ($q < 0$): Gyrate in a clockwise sense (right-handed rotation).

Because an orbiting charge forms an infinitesimal circular current loop $I = q (\omega_c / 2\pi)$, the magnetic dipole moment $\vec{\mu} = I \vec{A}$ produced by the orbiting particle is directed opposite to the background magnetic field $\vec{B}$ for both ions and electrons:

$$\vec{\mu} = -\frac{m v_\perp^2}{2 B^2} \vec{B}$$

Consequently, a plasma of gyrating particles is fundamentally diamagnetic: particle gyration naturally generates an opposing internal magnetic field that reduces the ambient $\vec{B}$.

§2.3 Motion in Orthogonal Uniform Electric and Magnetic Fields (E perp B)

1. Coupled Equations of Motion

Now introduce a static, uniform electric field perpendicular to $\vec{B}$. Let $\vec{B} = B_0 \hat{z}$ and $\vec{E} = E_y \hat{y}$. The Lorentz equations of motion become:

$$m \frac{dv_x}{dt} = q B_0 v_y, \quad m \frac{dv_y}{dt} = q E_y - q B_0 v_x, \quad m \frac{dv_z}{dt} = 0$$

Differentiating the $x$-equation with respect to time:

$$\frac{d^2 v_x}{dt^2} = \frac{q B_0}{m}\frac{dv_y}{dt} = \frac{q B_0}{m}\left[ \frac{q E_y}{m} - \frac{q B_0}{m}v_x \right] = -\omega_c^2 \left( v_x - \frac{E_y}{B_0} \right)$$

Defining a shifted velocity coordinate $u_x \equiv v_x - \frac{E_y}{B_0}$:

$$\frac{d^2 u_x}{dt^2} + \omega_c^2 u_x = 0$$

This demonstrates that in the moving reference frame, the particle undergoes ordinary cyclotron gyration around a guiding center translating steadily along the $+x$-axis with constant velocity:

$$v_E = \frac{E_y}{B_0}$$

§2.4 Derivation of the Guiding Center E x B Drift Velocity & Absence of Current

1. General Vector Derivation of E x B Drift

To derive the guiding center drift velocity in general coordinate-free vector form, partition the particle velocity $\vec{v}$ into a slowly varying guiding center drift velocity $\vec{v}_E$ and a rapidly oscillating gyration velocity $\vec{v}_c$:

$$\vec{v} = \vec{v}_E + \vec{v}_c$$

Averaging the Lorentz force equation over one complete cyclotron gyration period $\tau_c = 2\pi / \omega_c$, the periodic gyration acceleration averages to zero: $\langle d\vec{v}_c / dt \rangle = 0$. For a steady drift ($d\vec{v}_E / dt = 0$):

$$0 = q \left( \vec{E} + \vec{v}_E \times \vec{B} \right)$$

Taking the vector cross product with $\vec{B}$ on both sides:

$$\vec{E} \times \vec{B} + (\vec{v}_E \times \vec{B}) \times \vec{B} = 0$$

Applying the vector triple product identity $(\vec{A}\times\vec{B})\times\vec{C} = (\vec{A}\cdot\vec{C})\vec{B} - (\vec{B}\cdot\vec{C})\vec{A}$:

$$(\vec{v}_E \times \vec{B}) \times \vec{B} = (\vec{v}_E \cdot \vec{B})\vec{B} - B^2 \vec{v}_E = -B^2 \vec{v}_{E,\perp}$$

Assuming the drift is purely perpendicular to $\vec{B}$ ($\vec{v}_E \cdot \vec{B} = 0$):

$$\vec{E} \times \vec{B} - B^2 \vec{v}_E = 0 \implies \vec{v}_E = \frac{\vec{E} \times \vec{B}}{B^2}$$

2. Fundamental Physical Properties of E x B Drift

The $\vec{E}\times\vec{B}$ drift possesses several remarkable physical properties:

  1. Charge Independence: The drift velocity $\vec{v}_E$ is completely independent of the sign of the electric charge $q$. Both positive ions and negative electrons drift in the identical direction with the identical velocity.
  2. Mass Independence: The drift velocity does not depend on the particle mass $m$. Protons, heavy impurities, and electrons all drift together.
  3. Absence of Net Electric Current: Because both species move in unison: $$\vec{J}_E = n_e q_e \vec{v}_{E,e} + n_i q_i \vec{v}_{E,i} = n_0 (-e) \vec{v}_E + n_0 (+e) \vec{v}_E = 0$$ The $\vec{E}\times\vec{B}$ drift produces zero net electric current in a quasi-neutral plasma.

§2.5 Generalized External Force Drifts: Gravitational, Centrifugal & Collisional Frictional Drifts

1. Generalized Guiding Center Force Drift

Any general non-electromagnetic force $\vec{F}$ (such as gravity $\vec{F}_g = m\vec{g}$ or centrifugal force $\vec{F}_c = m v_\parallel^2 \hat{R}_c / R_c$) acting on a charged particle can be represented by an effective electric field:

$$\vec{E}_{\text{eff}} = \frac{\vec{F}}{q}$$

Substituting $\vec{E}_{\text{eff}}$ into the drift formula yields the generalized force drift velocity $\vec{v}_F$:

$$\vec{v}_F = \frac{\vec{E}_{\text{eff}} \times \vec{B}}{B^2} = \frac{1}{q} \frac{\vec{F} \times \vec{B}}{B^2}$$

2. Gravitational Drift

For a constant gravitational acceleration $\vec{g}$:

$$\vec{v}_g = \frac{m}{q} \frac{\vec{g} \times \vec{B}}{B^2}$$

Crucially, because of the explicit factor of $q$ in the denominator:

  • Ions and electrons drift in opposite directions!
  • Because $m_i \gg m_e$, the ion gravitational drift velocity is larger than the electron drift velocity by the mass ratio $M_i / m_e \approx 1836$.
  • This opposite motion establishes a net macroscopic cross-field electric current density: $$\vec{J}_g = n_0 e (\vec{v}_{gi} - \vec{v}_{ge}) \approx n_0 (M_i + m_e) \frac{\vec{g}\times\vec{B}}{B^2} \approx \rho_m \frac{\vec{g}\times\vec{B}}{B^2}$$ where $\rho_m = n_0 M_i$ is the mass density of the plasma.

§2.6 Time-Varying Electric Fields: Derivation of the Polarization Drift Velocity v_p

1. Inertial Lag in Time-Varying Fields

Consider a slowly time-varying electric field $\vec{E}(t) \perp \vec{B}_0$, where the rate of change is much slower than the cyclotron frequency:

$$\omega \ll \omega_c \iff \left| \frac{1}{E}\frac{dE}{dt} \right| \ll \omega_c$$

As $\vec{E}$ changes, the guiding center $\vec{E}\times\vec{B}$ drift velocity $\vec{v}_E(t) = \frac{\vec{E}(t)\times\vec{B}}{B^2}$ must also accelerate with time:

$$\frac{d\vec{v}_E}{dt} = \frac{1}{B^2}\left( \frac{d\vec{E}}{dt} \times \vec{B} \right)$$

Because the particle possesses finite mass $m$, inertia resists this acceleration. The particle experiences an effective inertial D'Alembert force:

$$\vec{F}_{\text{inertial}} = -m \frac{d\vec{v}_E}{dt} = -\frac{m}{B^2}\left( \frac{d\vec{E}}{dt} \times \vec{B} \right)$$

2. The Polarization Drift Velocity

This inertial force drives an additional guiding center drift according to the general force drift formula:

$$\vec{v}_p = \frac{1}{q}\frac{\vec{F}_{\text{inertial}} \times \vec{B}}{B^2} = -\frac{m}{q B^4}\left[ \left( \frac{d\vec{E}}{dt} \times \vec{B} \right) \times \vec{B} \right]$$

Applying the vector triple product identity $(\vec{A}\times\vec{B})\times\vec{B} = -B^2 \vec{A}_\perp$:

$$\vec{v}_p = -\frac{m}{q B^4} \left( -B^2 \frac{d\vec{E}_\perp}{dt} \right) = \frac{m}{q B^2} \frac{d\vec{E}_\perp}{dt}$$

This is the polarization drift velocity. Notice the critical features:

  • $\vec{v}_p$ is parallel to the changing electric field $\frac{d\vec{E}_\perp}{dt}$.
  • $\vec{v}_p$ is proportional to particle mass $m$. Because $M_i \gg m_e$, polarization drift is overwhelmingly an ion phenomenon: $\vec{v}_{pi} \gg \vec{v}_{pe}$.
  • $\vec{v}_p$ depends on charge $q$; ions and electrons drift in opposite directions, causing physical charge separation (polarization of the plasma).

§2.7 Polarization Current Density & The Effective Dielectric Permittivity of Magnetized Plasma

1. The Polarization Current Density

Because positive ions and negative electrons drift in opposite directions along $\frac{d\vec{E}}{dt}$, the polarization drift creates a net macroscopic current density, termed the polarization current $\vec{J}_p$:

$$\vec{J}_p = n_0 e (\vec{v}_{pi} - \vec{v}_{pe}) = n_0 e \left( \frac{M_i}{e B^2}\frac{d\vec{E}}{dt} - \frac{m_e}{-e B^2}\frac{d\vec{E}}{dt} \right) = \frac{n_0(M_i + m_e)}{B^2}\frac{d\vec{E}}{dt}$$

Defining the total mass density $\rho_m \equiv n_0(M_i + m_e) \approx n_0 M_i$:

$$\vec{J}_p = \frac{\rho_m}{B^2} \frac{d\vec{E}}{dt}$$

2. Dielectric Permittivity & Plasma Capacitance

In Maxwell's Ampère-Maxwell law, the total transverse current is the sum of conduction current, polarization current, and vacuum displacement current:

$$\nabla \times \vec{B} = \mu_0 \left( \vec{J} + \varepsilon_0 \frac{\partial \vec{E}}{\partial t} \right) = \mu_0 \left( \vec{J}_p + \varepsilon_0 \frac{\partial \vec{E}}{\partial t} \right) = \mu_0 \left( \frac{\rho_m}{B^2} + \varepsilon_0 \right) \frac{\partial \vec{E}}{\partial t}$$

The combined term acts as an effective displacement current in a medium with effective permittivity $\varepsilon$:

$$\varepsilon \equiv \varepsilon_0 + \frac{\rho_m}{B^2} = \varepsilon_0 \left( 1 + \frac{\rho_m}{\varepsilon_0 B^2} \right)$$

Recalling the definition of the Alfvén speed $v_A \equiv \frac{B}{\sqrt{\mu_0 \rho_m}}$, and noting $c^2 = 1/(\mu_0 \varepsilon_0)$:

$$\frac{\rho_m}{\varepsilon_0 B^2} = \frac{\rho_m \mu_0 c^2}{B^2} = \frac{c^2}{v_A^2}$$

Thus, the low-frequency relative dielectric constant (dielectric permittivity) $\epsilon_r$ of a magnetized plasma is:

$$\epsilon_r = \frac{\varepsilon}{\varepsilon_0} = 1 + \frac{c^2}{v_A^2}$$

In typical laboratory fusion and space plasmas where $v_A \ll c$ (e.g., $v_A \sim 10^6\text{ m/s}$), the dielectric constant is enormous: $\epsilon_r \sim 10^4 \text{ to } 10^6$. The magnetized plasma acts as an immense energy storage capacitor.

Honors Examination Worked Problems & Solutions

Rigorous step-by-step mathematical proofs and solutions to university degree examination problems.

Advanced Honors Exam Problem Example 2.1: Complete Analytical Integration of Cyclotron Trajectory in Crossed E x B Fields from First Principles

A singly ionized ion of mass $m$ and charge $q > 0$ is released from rest at the origin $\vec{r}(0) = 0$ at $t = 0$ in static uniform fields $\vec{E} = E_0 \hat{y}$ and $\vec{B} = B_0 \hat{z}$. (a) Set up the differential equations of motion for $v_x(t)$ and $v_y(t)$. (b) Solve analytically for the velocity vector $\vec{v}(t)$ using Laplace transforms or decoupling, and identify the guiding center drift velocity $v_E$. (c) Integrate the velocity to obtain the parametric trajectory $(x(t), y(t))$ in the $xy$-plane. (d) Identify the geometric nature of the curve and determine the maximum excursion $y_{\text{max}}$ in the direction of the electric field.

Full Rigorous Analytical Solution

(a) Equations of Motion: The Lorentz force equation is $m \frac{d\vec{v}}{dt} = q(\vec{E} + \vec{v}\times\vec{B})$. With $\vec{E} = (0, E_0, 0)$ and $\vec{B} = (0, 0, B_0)$:

$$\vec{v}\times\vec{B} = \det\begin{pmatrix} \hat{x} & \hat{y} & \hat{z} \\ v_x & v_y & v_z \\ 0 & 0 & B_0 \end{pmatrix} = (v_y B_0)\hat{x} - (v_x B_0)\hat{y}$$

Component equations:

  1. $m \dot{v}_x = q B_0 v_y \implies \dot{v}_x = \omega_c v_y$
  2. $m \dot{v}_y = q E_0 - q B_0 v_x \implies \dot{v}_y = \frac{q E_0}{m} - \omega_c v_x$
  3. $m \dot{v}_z = 0 \implies v_z(t) = v_z(0) = 0$

where $\omega_c = q B_0 / m$ is the cyclotron frequency.

(b) Velocity Solution: Differentiating the second equation:

$$\ddot{v}_y = -\omega_c \dot{v}_x = -\omega_c (\omega_c v_y) = -\omega_c^2 v_y$$

The general solution for $v_y(t)$ is:

$$v_y(t) = C_1 \cos(\omega_c t) + C_2 \sin(\omega_c t)$$

Given the initial condition $v_y(0) = 0$:

$$v_y(0) = C_1 = 0 \implies v_y(t) = C_2 \sin(\omega_c t)$$

From the equation of motion for $\dot{v}_y$ at $t = 0$:

$$\dot{v}_y(0) = \omega_c C_2 = \frac{q E_0}{m} - \omega_c v_x(0) = \frac{q E_0}{m} \implies C_2 = \frac{q E_0}{m \omega_c} = \frac{E_0}{B_0}$$

Therefore:

$$v_y(t) = \frac{E_0}{B_0} \sin(\omega_c t)$$

Now substitute $v_y(t)$ into the $\dot{v}_x$ equation:

$$\dot{v}_x = \omega_c \frac{E_0}{B_0} \sin(\omega_c t)$$

Integrating with initial condition $v_x(0) = 0$:

$$v_x(t) = -\frac{E_0}{B_0}\cos(\omega_c t) + C_3$$
$$v_x(0) = -\frac{E_0}{B_0} + C_3 = 0 \implies C_3 = \frac{E_0}{B_0}$$
$$v_x(t) = \frac{E_0}{B_0}\left[ 1 - \cos(\omega_c t) \right]$$

The constant term represents the guiding center $\vec{E}\times\vec{B}$ drift velocity:

$$v_E = \frac{E_0}{B_0}$$

(c) Parametric Spatial Trajectory: Integrate $v_x(t)$ with $x(0) = 0$:

$$x(t) = \int_0^t v_x(t') dt' = \frac{E_0}{B_0} \int_0^t [1 - \cos(\omega_c t')] dt' = \frac{E_0}{B_0}\left[ t - \frac{\sin(\omega_c t)}{\omega_c} \right]$$

Integrate $v_y(t)$ with $y(0) = 0$:

$$y(t) = \int_0^t v_y(t') dt' = \frac{E_0}{B_0} \int_0^t \sin(\omega_c t') dt' = \frac{E_0}{\omega_c B_0}\left[ 1 - \cos(\omega_c t) \right]$$

Defining the radius $R_c = \frac{E_0}{\omega_c B_0} = \frac{m E_0}{q B_0^2}$:

$$x(t) = R_c (\omega_c t - \sin(\omega_c t)), \quad y(t) = R_c (1 - \cos(\omega_c t))$$

(d) Geometric Curve & Maximum Excursion: These parametric equations represent a standard cycloid generated by a circle of radius $R_c$ rolling without slipping along the $x$-axis at velocity $v_E = R_c \omega_c = E_0 / B_0$. The maximum excursion in the $y$-direction occurs when $\cos(\omega_c t) = -1$ (at $\omega_c t = \pi, 3\pi, \dots$):

$$y_{\text{max}} = 2 R_c = \frac{2 m E_0}{q B_0^2}$$

At this peak, the particle's velocity is entirely in the $+x$-direction with magnitude $v_x = 2 E_0 / B_0$.

Final Answer & Physical Verification

Complete rigorous derivation and proof detailed above.

Final Answer & Physical Insight

Complete rigorous derivation and proof detailed above.

Advanced Honors Exam Problem Example 2.2: Relativistic Gyro-Radius and Synchrotron Pitch Angle Kinematics in High-Magnetic-Field Laboratory Environments

A relativistic electron with total kinetic energy $T_e = 5.0\text{ MeV}$ is injected into a uniform magnetic field $B_0 = 4.0\text{ Tesla}$ with pitch angle $\alpha = 60^\circ$ relative to $\vec{B}_0$. (a) Compute the relativistic Lorentz factor $\gamma$, total energy $E$, and momentum magnitude $p$ of the electron. (b) Calculate the relativistic cyclotron frequency $\omega_{c,\text{rel}}$ and the relativistic Larmor radius $r_{L,\text{rel}}$. (c) Compare these relativistic values with the naive non-relativistic formulas and compute the percentage discrepancy. (d) Calculate the longitudinal distance $\Delta z$ traversed along $\vec{B}_0$ in one full gyration period.

Full Rigorous Analytical Solution

(a) Relativistic Energy & Momentum: Electron rest mass energy is $m_e c^2 = 0.511\text{ MeV}$. Total relativistic energy:

$$E = T_e + m_e c^2 = 5.0\text{ MeV} + 0.511\text{ MeV} = 5.511\text{ MeV}$$

Lorentz factor $\gamma$:

$$\gamma = \frac{E}{m_e c^2} = \frac{5.511\text{ MeV}}{0.511\text{ MeV}} \approx 10.785$$

Total momentum $p$:

$$p c = \sqrt{E^2 - (m_e c^2)^2} = \sqrt{(5.511)^2 - (0.511)^2} = \sqrt{30.371 - 0.261} = \sqrt{30.110} \approx 5.487\text{ MeV}$$
$$p = \frac{5.487 \times 10^6 \times 1.6022\times 10^{-19}\text{ J}}{2.9979\times 10^8\text{ m/s}} = 2.932 \times 10^{-21}\text{ kg}\cdot\text{m/s}$$

Perpendicular momentum component with pitch angle $\alpha = 60^\circ$:

$$p_\perp = p \sin(60^\circ) = (2.932\times 10^{-21}) \times 0.8660 = 2.539 \times 10^{-21}\text{ kg}\cdot\text{m/s}$$

Parallel momentum component:

$$p_\parallel = p \cos(60^\circ) = (2.932\times 10^{-21}) \times 0.500 = 1.466 \times 10^{-21}\text{ kg}\cdot\text{m/s}$$

(b) Relativistic Cyclotron Frequency & Larmor Radius: In relativistic dynamics, the relativistic mass is $\gamma m_e$. Relativistic cyclotron frequency:

$$\omega_{c,\text{rel}} = \frac{e B_0}{\gamma m_e} = \frac{\omega_{c0}}{\gamma}$$

Non-relativistic gyrofrequency $\omega_{c0}$:

$$\omega_{c0} = \frac{(1.6022\times 10^{-19})(4.0)}{9.109\times 10^{-31}} = 7.036 \times 10^{11}\text{ rad/s}$$
$$\omega_{c,\text{rel}} = \frac{7.036 \times 10^{11}}{10.785} = 6.524 \times 10^{10}\text{ rad/s}$$

Relativistic Larmor radius:

$$r_{L,\text{rel}} = \frac{p_\perp}{e B_0} = \frac{2.539 \times 10^{-21}\text{ kg}\cdot\text{m/s}}{(1.6022\times 10^{-19}\text{ C})(4.0\text{ T})} = 3.962 \times 10^{-3}\text{ m} \approx 3.96\text{ mm}$$

(c) Comparison with Non-Relativistic Values: Naive non-relativistic calculation would use $v_\perp = \sqrt{2 T_e / m_e}$, which exceeds the speed of light ($v > c$), giving an erroneous gyrofrequency:

$$\omega_{c,\text{naive}} = 7.036 \times 10^{11}\text{ rad/s}$$

The true relativistic frequency is smaller by a factor of $\gamma = 10.785$ (a factor of over 10 reduction, or $-90.7\%$ discrepancy). The relativistic Larmor radius $r_{L,\text{rel}}$ is enlarged by a factor of $\gamma$ relative to the momentum scaling, emphasizing that relativistic inertia dramatically expands gyro-orbits.

(d) Longitudinal Distance per Gyration: The gyration period is:

$$\tau_c = \frac{2\pi}{\omega_{c,\text{rel}}} = \frac{2\pi}{6.524\times 10^{10}} = 9.63 \times 10^{-11}\text{ s}$$

The parallel velocity is $v_\parallel = \frac{p_\parallel}{\gamma m_e} = \frac{1.466\times 10^{-21}}{10.785 \times 9.109\times 10^{-31}} = 1.492 \times 10^8\text{ m/s} \approx 0.498 c$. The pitch advance distance per gyration loop is:

$$\Delta z = v_\parallel \tau_c = (1.492\times 10^8\text{ m/s}) \times (9.63\times 10^{-11}\text{ s}) = 1.437 \times 10^{-2}\text{ m} = 1.44\text{ cm}$$
Final Answer & Physical Verification

Complete rigorous derivation and proof detailed above.

Final Answer & Physical Insight

Complete rigorous derivation and proof detailed above.

Advanced Honors Exam Problem Example 2.3: Derivation of Polarization Current Density and Effective Low-Frequency Dielectric Permittivity for Alfvenic Fields

A slab of hydrogen plasma (protons $M_i = 1.673\times 10^{-27}\text{ kg}$, electrons $m_e = 9.109\times 10^{-31}\text{ kg}$, density $n_0 = 5.0\times 10^{19}\text{ m}^{-3}$) is embedded in a static magnetic field $\vec{B}_0 = 2.0\text{ T} \hat{z}$. A linearly ramped transverse electric field $\vec{E}(t) = (E_0 t / \tau) \hat{x}$ is applied across the plasma for $0 \le t \le \tau$, where $E_0 = 10.0\text{ kV/m}$ and $\tau = 1.0\;\mu\text{s}$. (a) Compute the polarization drift velocity for ions $\vec{v}_{pi}$ and electrons $\vec{v}_{pe}$. (b) Calculate the resulting polarization current density $\vec{J}_p$. (c) Determine the Alfvén velocity $v_A$ and the low-frequency relative dielectric constant $\epsilon_r$ of the plasma. (d) Compute the total electric charge per unit area accumulated on the plasma boundary faces perpendicular to $\hat{x}$ by time $t = \tau$.

Full Rigorous Analytical Solution

(a) Polarization Drift Velocities: The electric field ramps linearly:

$$\frac{d\vec{E}}{dt} = \frac{E_0}{\tau}\hat{x} = \frac{10^4\text{ V/m}}{10^{-6}\text{ s}}\hat{x} = 1.0 \times 10^{10}\text{ V}/(\text{m}\cdot\text{s})\hat{x}$$

The polarization drift formula is:

$$\vec{v}_{p} = \frac{m}{q B_0^2} \frac{d\vec{E}}{dt}$$

1. For Ions ($q = +e, m = M_i$):

$$v_{pi} = \frac{M_i}{e B_0^2}\frac{dE}{dt} = \frac{1.673\times 10^{-27}\text{ kg}}{(1.6022\times 10^{-19}\text{ C})(2.0\text{ T})^2}(1.0\times 10^{10}\text{ V/ms}) = \frac{1.673\times 10^{-17}}{6.409\times 10^{-19}} \approx 26.1\text{ m/s}$$
$$\vec{v}_{pi} = +26.1\hat{x}\text{ m/s}$$

2. For Electrons ($q = -e, m = m_e$):

$$v_{pe} = \frac{m_e}{-e B_0^2}\frac{dE}{dt} = -\frac{9.109\times 10^{-31}}{(1.6022\times 10^{-19})(4.0)}(1.0\times 10^{10}) = -1.42 \times 10^{-2}\text{ m/s}$$
$$\vec{v}_{pe} = -0.0142\hat{x}\text{ m/s}$$

Notice that $\vec{v}_{pi} / |\vec{v}_{pe}| = M_i / m_e \approx 1836$: the ions completely dominate the physical mass transport.

(b) Polarization Current Density $\vec{J}_p$:

$$\vec{J}_p = n_0 e (\vec{v}_{pi} - \vec{v}_{pe}) = \frac{n_0 (M_i + m_e)}{B_0^2}\frac{d\vec{E}}{dt} \approx \frac{\rho_m}{B_0^2}\frac{d\vec{E}}{dt}$$

Mass density $\rho_m$:

$$\rho_m = n_0 M_i = (5.0\times 10^{19}\text{ m}^{-3})(1.673\times 10^{-27}\text{ kg}) = 8.365 \times 10^{-8}\text{ kg/m}^3$$

Evaluating $\vec{J}_p$:

$$J_p = \frac{8.365\times 10^{-8}\text{ kg/m}^3}{(2.0\text{ T})^2} \times (1.0\times 10^{10}\text{ V/ms}) = (2.091\times 10^{-8}) \times 10^{10} = 209.1\text{ A/m}^2$$
$$\vec{J}_p = +209.1\hat{x}\text{ A/m}^2$$

(c) Alfvén Speed $v_A$ & Relative Permittivity $\epsilon_r$: Alfvén speed:

$$v_A = \frac{B_0}{\sqrt{\mu_0 \rho_m}} = \frac{2.0}{\sqrt{(4\pi\times 10^{-7})(8.365\times 10^{-8})}} = \frac{2.0}{\sqrt{1.051\times 10^{-13}}} = \frac{2.0}{3.242\times 10^{-7}} = 6.169 \times 10^6\text{ m/s}$$

Relative dielectric permittivity:

$$\epsilon_r = 1 + \frac{c^2}{v_A^2} = 1 + \frac{(2.998\times 10^8)^2}{(6.169\times 10^6)^2} = 1 + (48.6)^2 = 1 + 2362 = 2363$$

The magnetized plasma has an effective dielectric constant of $\epsilon_r \approx 2363$, demonstrating immense capacitive polarizability.

(d) Accumulated Boundary Surface Charge Density: Because the current $J_p$ is steady over the time interval $\Delta t = \tau = 1.0\;\mu\text{s}$:

$$\sigma_{\text{pol}} = \int_0^\tau J_p dt = J_p \tau = (209.1\text{ A/m}^2)(1.0\times 10^{-6}\text{ s}) = 2.091 \times 10^{-4}\text{ C/m}^2 = 209.1\;\mu\text{C/m}^2$$

This surface charge density creates a macroscopic internal polarization electric field opposing the external applied field, analogous to a dielectric capacitor.

Final Answer & Physical Verification

Complete rigorous derivation and proof detailed above.

Final Answer & Physical Insight

Complete rigorous derivation and proof detailed above.