Dynamics of a charged particle in a linearly polarized traveling electromagnetic wave

A model of a scalar particle in (2+1)-dimensional space with an internal structure in external electromagnetic fields is considered. Exact solutions of the equation for such scalar particle were obtained in the field of a plane electromagnetic wave with the arbitrary polarization and in the quantized electromagnetic field of the linearly polarized wave. The relativistic coherent states of the particle in the field of n photons were constructed. When the photon number goes to infinity, this wave function transforms to the solution corresponding to the external classical electromagnetic wave.

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Canonical form of the averaged equations of motion of a charged particle upon superposition of an electromagnetic wave field on a weakly inhomogeneous magnetic field

Physics of the Solid State ◽

10.1134/1.1434474 ◽

2002 ◽

Vol 44 (1) ◽

pp. 4-7 ◽

Cited By ~ 1

Author(s):

V. E. Tarasov ◽

K. Sh. Khodzhaev ◽

A. G. Chirkov

Keyword(s):

Magnetic Field ◽

Electromagnetic Wave ◽

Charged Particle ◽

Wave Field ◽

Canonical Form ◽

Equations Of Motion ◽

Inhomogeneous Magnetic Field ◽

Averaged Equations ◽

Electromagnetic Wave Field

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Emission Spectrum and Charged-Particle Trajectory in the Field of an Inhomogeneous Electromagnetic Wave

Doklady Physics ◽

10.1134/s1028335819100070 ◽

2019 ◽

Vol 64 (10) ◽

pp. 377-380

Author(s):

V. B. Lapshin ◽

A. A. Skubachevskiy ◽

A. V. Belinsky ◽

A. S. Bugaev

Keyword(s):

Electromagnetic Wave ◽

Charged Particle ◽

Emission Spectrum ◽

Particle Trajectory ◽

Inhomogeneous Electromagnetic Wave

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Dynamics of a charged particle in a linearly polarized traveling wave, Hamiltonian approach to laser-matter interaction at very high intensities

The 30th International Conference on Plasma Science, 2003. ICOPS 2003. IEEE Conference Record - Abstracts. ◽

10.1109/plasma.2003.1228645 ◽

2003 ◽

Author(s):

A. Bourdier ◽

D. Patin

Keyword(s):

Charged Particle ◽

Traveling Wave ◽

Hamiltonian Approach ◽

Matter Interaction ◽

Linearly Polarized ◽

Very High

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Dynamics of a charged particle in a linearly polarized traveling wave: applications to laser-matter interaction at very high intensities

IEEE Conference Record - Abstracts 2002 IEEE International Conference on Plasma Science (Cat No 02CH37340) PLASMA-02 ◽

10.1109/plasma.2002.1030447 ◽

2003 ◽

Author(s):

A. Bourdier

Keyword(s):

Charged Particle ◽

Traveling Wave ◽

Matter Interaction ◽

Linearly Polarized ◽

Very High

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First and second order approximations of the first adiabatic invariant for a charged particle interacting with a linearly polarized hydromagnetic plane wave

Planetary and Space Science ◽

10.1016/0032-0633(77)90128-3 ◽

1977 ◽

Vol 25 (8) ◽

pp. 765-771

Author(s):

R. Vanclooster

Keyword(s):

Charged Particle ◽

Plane Wave ◽

Second Order ◽

Adiabatic Invariant ◽

Linearly Polarized

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Effect of Anisotropic Characteristics of Composite Skins on the Electromagnetic Wave Propagation in the Foam Core Sandwich Structures

International Journal of Modern Physics B ◽

10.1142/s0217979203019666 ◽

2003 ◽

Vol 17 (08n09) ◽

pp. 1782-1787 ◽

Cited By ~ 1

Author(s):

Heoung Jae Chun ◽

Hyun Su Shin

Keyword(s):

Electromagnetic Wave ◽

Fiber Orientation ◽

Electromagnetic Waves ◽

Composite Laminate ◽

Electromagnetic Wave Propagation ◽

Sandwich Structures ◽

Incident Angle ◽

Foam Core ◽

Linearly Polarized ◽

Composite Skins

The propagation of electromagnetic waves in the foam core sandwich structures is highly affected by anisotropic permittivity and loss tangent of composite skins. Even though many investigations were focused on the propagation of electromagnetic waves in the composite materials in last several decades, little investigations were carried out to understand adequately the propagation of the electromagnetic waves in the foam core sandwich structures. In this study, the transmittance of the arbitrary linearly polarized incident TEM waves through the solid composite laminate with various stacking sequences and foam core sandwich structures with composite skins was calculated as functions of fiber orientation of composites and incident angle of the wave by the analytical model.

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