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# Pulse Propagation

Consider the situation, studied in Section 6.3, in which a plane wave, polarized in the -direction, is launched along the -axis, from an antenna located at large positive , and reflected from a cutoff located at . Up to now, we have only considered infinite wave-trains, characterized by a discrete frequency, . Let us now consider the more realistic case in which the antenna emits a finite pulse of radio waves.

The pulse structure is conveniently represented as

 (6.70)

where is the electric field produced by the antenna, which is assumed to lie at . Suppose that the pulse is a signal of roughly constant (angular) frequency , which lasts a time , where is long compared to . It follows that possesses narrow maxima around . In other words, only those frequencies that lie very close to the central frequency, , play a significant role in the propagation of the pulse.

Each component frequency of the pulse yields a wave that propagates independently along the -axis, in a manner specified by the appropriate WKB solution [see Equations (6.17) and (6.18)]. Thus, if Equation (6.70) specifies the signal at the antenna (i.e., at ) then the signal at coordinate (where ) is given by

 (6.71)

where

 (6.72)

Here, we have made use of the fact that .

Equation (6.71) can be regarded as a contour integral in -space. The quantity is a relatively slowly varying function of , whereas the phase, , is a large and rapidly varying function of . The rapid oscillations of over most of the path of integration ensure that the integrand averages almost to zero. However, this cancellation argument does not apply to places on the integration path where the phase is stationary: that is, places where has an extremum. The integral can, therefore, be estimated by finding those points where has a vanishing derivative, evaluating (approximately) the integral in the neighborhood of each of these points, and summing the contributions. This procedure is called the method of stationary phase (Budden 1985).

Suppose that has a vanishing first derivative at . In the neighborhood of this point, can be expanded as a Taylor series,

 (6.73)

Here, the subscript is used to indicate or its second derivative evaluated at . Because is slowly varying, the contribution to the integral from this stationary phase point is approximately

 (6.74)

The previous expression can be written in the form

 (6.75)

where

 (6.76)

The integrals in the previous expression are known as Fresnel integrals (Abramowitz and Stegun 1965b), and can be shown to take the values

 (6.77)

It follows that

 (6.78)

If there is more than one point of stationary phase in the range of integration then the integral is approximated as a sum of terms similar to that in the previous formula.

Integrals of the form (6.71) can be calculated exactly using the method of steepest descent (Brillouin 1960; Budden 1985). The stationary phase approximation (6.78) agrees with the leading term of the method of steepest descent (which is far more difficult to implement than the method of stationary phase) provided that is real (i.e., provided that the stationary point lies on the real axis). If is complex, however, then the stationary phase method can yield erroneous results.

It follows, from the previous discussion, that the right-hand side of Equation (6.71) averages to a very small value, expect for those special values of and at which one of the points of stationary phase in -space coincides with one of the peaks of . The locus of these special values of and can obviously be regarded as the equation of motion of the pulse as it propagates along the -axis. Thus, the equation of motion is specified by

 (6.79)

which yields

 (6.80)

Suppose that the -velocity of a pulse of central frequency at coordinate is given by . The differential equation of motion of the pulse is then . This can be integrated, using the boundary condition at , to give the full equation of motion:

 (6.81)

A comparison of Equations (6.80) and (6.81) yields

 (6.82)

The velocity is usually called the group-velocity. It is easily demonstrated that the previous expression for the group-velocity is entirely consistent with that given in Equation (5.72).

The dispersion relation for an electromagnetic plasma wave propagating through an unmagnetized plasma is [see Equation (6.121)]

 (6.83)

Here, we have assumed that equilibrium quantities are functions of only, and that the wave propagates along the -axis. The phase-velocity of waves of frequency propagating along the -axis is given by

 (6.84)

According to Equations (6.82) and (6.83), the corresponding group-velocity is

 (6.85)

It follows that

 (6.86)

Let us assume that , and for , which implies that the reflection point corresponds to . It is clear from Equations (6.84) and (6.85) that the phase-velocity of the wave is always greater than the velocity of light in vacuum, whereas the group-velocity is always less than this velocity. Furthermore, as the reflection point, , is approached from positive , the phase-velocity tends to infinity, whereas the group-velocity tends to zero.

Although we have only analyzed the motion of the pulse as it travels from the antenna to the reflection point, it is easily demonstrated that the speed of the reflected pulse at position is the same as that of the incident pulse. In other words, the group velocities of pulses traveling in opposite directions are of equal magnitude.

Next: Ray Tracing Up: Wave Propagation Through Inhomogeneous Previous: Collisional Damping
Richard Fitzpatrick 2016-01-23