Starting with the principle of superposition, the electric field intensity at a particular point in space is generated by the various fields, E1, E2, ..., of the constituent sources,
For the sake of simplicity, consider two point sources, S1 and S2, emitting monochromatic waves of the same frequency in a homogenous medium. Let their separation a be much greater than . Locate the point of observation, P, far enough away from the sources so that at P the wavefronts will be planes. For now, consider only linearly polarized waves of the form
The irradiance at P is given by
Recognizing that is the time average of the square of the magnitude of the electric field intensity, we see that
The last term is known as the interference term. For the waves described by (13.2) and (13.3), this can be evaluated as follows. First, consider the effect of :
Recall that the time average of a function f(t), taken over an interval T, is
where we used the fact that , , and . The interference term is then
where is the phase difference. It comes from the combined path length and the initial phase angle difference.
We can simplify our results in the case of parallel amplitudes, . In this case, equation (13.8) reduces to . (13.9)
Using the fact that
so that the total irradiance becomes
This reaches a maximum value of
when , where . In this case the distributions are said to be in phase. This is known as total constructive interference. When 0 < cos < 1, the waves are out of phase, I1 + I2 < I < Imax, and the condition is known as constructive interference. At , cos = 0, the optical disturbances are said to be 90 out of phase. For 0 > cos > -1 we get destructive interference, I1 + I2 > I > Imin. The minimum occurs when
when , where . This is known as total destructive interference.
Another special case is when the amplitudes of both waves are equal. In this case the irradiances from both sources are equal, so let I1 = I2 = I0. Equation (13.11) can then be written as
from which it follows that Imin = 0 and Imax = 4I0.
We have now discussed how two waves overlap to create an interference, or fringe, pattern. In order for this pattern to be observed, the two sources do not need to be in phase with each other. If there is some constant initial phase difference between the two sources, the resulting interference pattern will be identical to the original pattern, although it will be shifted in terms of the location of the minima and maxima. Such sources are said to be coherent. Remember that conventional quasimonochromatic sources produce light which is a mix of photon wavetrains. At each illuminated point in space there is a net field which oscillates through approximately a million cycles, which averages 10 ns or less, before it randomly changes phase. This interval over which the light wave resembles a sine function is a measure of its temporal coherence. Since the average time interval during which the wavetrain oscillates in a predictable manner is given by the coherence time, we see that the longer the coherence time, the greater the temporal coherence of the source. In a similar way, if we observe the light wave from a fixed point in space, we see that it appears to be fairly sinusoidal for some number of oscillations between abrupt phase changes. The corresponding spatial extent over which the light wave oscillates in a regular, predictable way has already been identified as the coherence length. If we view the light beam as a progression of well defined sinusoidal wavegroups of average length xC, whose phases are uncorrelated to one another, then we find that normal coherence lengths range from several millimeters for standard laboratory discharge tubes up to tens of kilometers for some lasers.
Two ordinary sources will normally maintain a constant relative phase for a time no greater than tC, so the interference pattern that they produce will randomly shift around in space at an extremely rapid rate, averaging out and making it impractical to observe. Until the advent of the laser, it was generally accepted that no two individual sources would ever produce an observable interference pattern. The coherence time of lasers, however, is long enough so that interference of two independent lasers has been detected electronically.
If two beams are to interfere to produce a stable pattern, they must have nearly the same frequency. A significant frequency difference would result in a rapidly varying time dependent phase difference, which would cause I12 to average out to zero during the detection interval. If the sources both emit white light, the component reds will interfere with the reds, and the blues with the blues. A great many overlapping monochromatic patterns will be produces which combine to create a total white light pattern. This final pattern will not be as sharp or extensive as a monochromatic pattern, but white light will produce observable interference.
In addition to situations in which two coherent beams are combined to produce interference patterns, there are circumstances in which a much larger quantity of mutually coherent waves are made to interfere. To begin analyzing such a system, consider a glass plate, slightly silvered on both sides so that the reflection coefficients, the r's, are near unity. Assume that the silver film, substrate, and surrounding medium are transparent dielectrics, and let the film be nonabsorbing. For simplicity, let n1 = n2; this avoids the necessity of introducing different reflection and transmission coefficients at each interface.
where is the incident wave.
The terms are the contributions to the phase arising from the optical path length difference between adjacent rays, . There is an additional phase contribution arising from the optical distance traversed in reaching point P, but this is common to each ray and thus can be ignored. The resultant reflected scalar wave is then
If , and if the number of terms in the series approaches infinity, the series converges to
The reflected flux density at P is
The amplitude of the transmitted waves are given by
These can be added to yield
In turn, this leads to the irradiance of the transmitted beam being given by
Using the identity , and setting , (13.18) and (13.21) can be rewritten as
The term is known as the Airy function, and is denoted A(). It represents the transmitted flux density distribution. The complementary function, [1 - A()] represents the reflected flux density distribution.