Before proceeding with a discussion of the mechanisms, it is worth once more contemplating the nature of the vertical beam. If the beam was indeed tilted off-vertical, then one can imagine specific scenarios in which the layer coincidentally forms perpendicular to the beam, so the layer appears “horizontal” as far as the radar is concerned. However, one can also envisage many more scenarios where the combined effects of the beam-direction and the layer orientation makes the calculation of the true layer orientation worse than it should be. In fact, it is to be expected that any error correction will be azimuthally dependent (for example, if the tilt is perpendicular to
ϕ0, there will be no bias) and that the net effect will be an integrated effect across all azimuthal angles available in the data. In general, it is to be expected that cases in which the beam’s direction and the layer tilt partially cancel out are the least common cases. While it may be possible to develop a detailed model of correction for beam tilts, it is clear that, in the worst case, the effect of the beam and the layer will add, and when averaged over multiple azimuths, will be less than additive but will still increase relative to the true value. Considering the worst-case scenario to be statistically additive between the layer and beam tilts, then the tilts shown in
Figure 7 and
Figure 8 should all exceed the actual vertical beam tilt. Therefore, the lowest values seen in
Figure 7 and
Figure 8 would be upper limits on the tilt of the vertical beam. Occurrences of a “layer-tilt” of 0.2° are moderately common in
Figure 7 and
Figure 8, and tilts of 0.2° to 0.4° are very common. Hence, we may conclude that all vertical radar beams are offset from vertical by less than 0.4° and very likely less than 0.2°. Other studies, also reported in [
32], looked for instrumental biases related to the azimuthal angles, and no biases were found. These further demonstrated that tilts in the main beam were of little consequence in our study (see table 6.1 in [
32]); so, henceforth we assume that all of the tilts that were measured were atmospheric in origin.
In addition, it is important to recall (again) that values of the maximum correlation coefficient ρM of less than 0.15 occurred for layers which were close to horizontal, and, in many ways, such occasions apply to the ideal situation of a perfectly horizontal layer; but the fact remains that such “ideal” situations are less common than might be naively expected. We will argue shortly that this anticipation of “flatness” may itself be a premature expectation.
Next, possible atmospheric causes of these tilts need to be considered. The discussion of these causes will be broken into subsections.
5.1. Linear (Un-Saturated) Gravity Waves
In this section, the possibility that linear gravity waves could reflect radio-waves at a detectable level is discussed. We do not include saturating or breaking waves here—these may be important but are discussed in a later section.
Recall from the Introduction of this paper that radio-waves are only reflected effectively from reflecting structures if the structures have significant Fourier components at the Bragg scale. This requires that either (i) the structures have sharp edges and that these edges are less than half of the radar wavelength in width, or that (ii) the scatterers are in fact sinusoidal with a wavelength along the beam equal to the Bragg wavelength, or that (iii) the scatterers are isolated entities with widths of the order of half of the radar wavelength (like the ellipsoids in
Figure 1). Viscosity waves were discussed as an example of case (ii) in the Introduction of this paper.
It has been proposed by [
33] that gravity waves might be able to satisfy this criterion, so we need to briefly address that possibility here. The proposal by [
33] was somewhat speculative, and, in the end, the authors concluded that, even if it could happen, the Bragg scales of the gravity waves could not be less than 20 m or so. The Bragg scales for our radars are all in the range 3 to 4 m, so this is not a feasible explanation for our results. Furthermore, [
16] analyzed the effects of viscosity on the gravity-wave equations and showed that this model was quite infeasible at our scale.
So the only way in which unsaturated gravity waves could cause significant reflections is through reflections from entities embedded inside the waves that are moved around by the waves. In the following paragraphs, we assume that pre-existing “tracers” cause the radio reflections and that the waves simply perturb them. It should also be noted that we use hourly averaged data, so the smallest waves that could be detected in the vertical motions will have period of 2 h and more; shorter period motions will be significantly dampened in our data. A discussion of the possibility that perturbations in linear gravity waves can lead to the correlations demonstrated in this paper now ensues.
Several points need to be noted. First, gravity waves have polarization relations between the horizontal and vertical components of the wave (e.g., [
34,
35] and [
20], equation (11.18)), so that horizontal and vertical wind components are in phase or in anti-phase. However, this effect is an additional effect on top of the mean wind; our studies have looked at correlations between the vertical velocities and the total mean horizontal winds, which is not the same thing. Furthermore, while the vertical and horizontal winds are well understood when they are measured at the same point in space, the radar measures horizontal winds using the off-vertical beams and the vertical wind on the vertical beam, and so each are measured at different times and different points in space. Therefore, any phase relationship depends on the wavelength and period of the wave. Even further, the ratio of vertical to horizontal velocity components becomes smaller as the period increases, and as discussed above, we used hourly averages, so any effects at periods less than 2 h (when vertical velocities are more dominant) are washed out. In addition, there may be many waves present at any one time, with different wavelengths, periods, and directions of travel. All in all, the effect of polarization relations of gravity waves will be diminished.
There is, however, one type of gravity wave for which the polarization relations between the vertical and horizontal velocities might have relevance for our studies. Lee waves, generated by flow over mountains, can produce steady-state conditions overhead of a radar close to the mountain (e.g., [
36], or [
20], figure 12.13). If a single wave were dominant, it is possible that it may lead to fixed tilts over the radar. But, over the course of a month, multiple waves may be generated, with different horizontal wavelengths, and these would produce varying layer-slopes in the scattering layers. If the mean wind changes direction, then the situation will also change; for some wind alignments, there will be no lee waves over the radar. Such a scenario involving lee-waves also requires a nearby mountain; most of our radars do not have nearby mountains. So, lee-waves cannot explain our results generally, although are likely to be relevant in some special circumstances.
In an interesting paper, [
37] has tried to simulate the anisotropy in power as a function of angle seen by the MU radar in Japan. They assumed linear gravity waves, and their
Figure 1 shows a schematic of radio-waves being reflected from a sinusoidal surface. They are careful to say that the “corrugated surface” presented in that figure is not due to gravity waves directly, but is caused by the “effects of gravity waves”; in other words, they are referring to “tracers” which are being orientated by linear gravity waves. Despite some success in replicating their own observations, they also recognized errors. However, their results did not offer anything that could explain the correlations shown in
Figure 2 of this paper; all of our comments above still apply. They did comment that as the waves saturate, and if horizontal velocities are included, then the waves take on a saw-tooth structure, which may be important—but that refers to non-linear waves, which will be discussed later.
Thus, unsaturated linear gravity waves cannot explain our long-term correlations. Other types of waves, like larger-scale planetary waves, have far gentler sloping isobaric tilts, and will produce angles comparable to those smaller slopes discussed at the end of the Introduction of this paper; so these waves cannot explain our results either.
Nevertheless, we have not finished with gravity waves yet, and we will return to a discussion of saturated and breaking waves, as well as Kelvin-Helmholtz billows, in
Section 5.5.
5.4. Small-Scale Reflectors and Scatterers
In
Section 5.1 and
Section 5.2, there was little mention of the lengths of the reflecting/scattering “tracers”. It is easy to believe that they might perhaps be hundreds of metres, or even kilometres, long, perhaps like
Figure 1a. But there is no reason that this should be so. To begin this section, let us return to
Figure 1e. This figure proposes that, within a patch of turbulence, ellipsoidal eddies form and that they have systematic tilts. In intense turbulence, there can be some questions about whether such eddies even exist, but they are frequently used in theoretical discussions of turbulence. To look at it another way, all atmospheric refractivity structures can be Fourier transformed, and radar back-scatter occurs from the Fourier components of length λ/2, aligned perpendicularly to the direction of travel of the radar wave. But we could equally mathematically decompose the entire refractivity structure into a collection of ellipsoids of different widths, lengths, and refractive indices, and base our modelling on the scatter from these ellipsoids (similarly to [
20], figure 7.18).
In order to broaden the scope, let us also assume that these ellipsoidal eddies could even be tilted refractive index structures analogous to “shards” of partially reflecting glass. If the shards are, say, ten wavelengths long, they can be thought of as little reflecting mirrors. If the length of the reflectors is only a few wavelengths, or even less, then it needs to be recalled that the back-scattered radiation will not be purely perpendicular, but will spread out in a manner proportional to the diffraction pattern of a hole (of the same size and shape of the shard) in an opaque screen (Babinet’s principle). We will be able to distinguish between the different models using an “anisotropy parameter”, which we will represent as θa, and which will be defined shortly.
In fact, in an important development, [
42] has shown that for cases of semi-transparent media (as here), the use of three-dimensional ellipsoidal structures with weak variations in refractive index relative to the background is equivalent to using flat weakly scattering quasi-reflectors (the “shards of glass”), possibly with “wrinkles”. The latter approach has commonly been used by [
3]. We will adopt this model of ellipsoidal refractive-index structures for our discussions.
Figure 1d assumes that the ellipsoids are aligned with their long axis horizontal, and even
Figure 1f assumes that the ellipsoids are, on average, horizontal. But is this reasonable? After all, the development of dynamic turbulence relies on the Richardson number being less than ~0.25, so it relies on the wind-shear dominating over stability. So if the effect of stability is reduced, then why should the mean alignment of the eddies have to be exactly horizontal?
Figure 1e becomes a better representation. Even better would be
Figure 1e with some random fluctuations super-imposed (like
Figure 1f). Indeed, the average tilt of the eddies might be partially defined by the wind shear, or some ratio of wind shear to buoyancy, or even by the Richardson number itself.
For now, we will consider the model shown in
Figure 1e as a basis, with some allowance for quasi-random fluctuation about the mean tilt like in
Figure 1f. As noted, we also allow for the tilted scatterers/reflectors to take various forms. As a further example, [
43] has proposed that tilted structures associated with Kelvin-Helmholtz Instabilities (KHI) could exist, and our following discussions will also cover that possibility. However, one advantage of the ellipsoid approach is that the ratios of the major to minor axis lengths can be found [
44,
45], and this gives a good physical parameter for specifying the degree of anisotropy.
The question now is the following: how will such a model affect the radar measurements? To answer this, we need to turn to
Figure 9. This figure shows a stream of tilted ellipsoids blowing through the beam. It is assumed that the wind is purely horizontal. In this case, we have used downward sloping eddies (mean alignment is shown by the sloping broken lines). This tilt direction is the opposite to
Figure 1e (downward here compared to upward there), but the concept remains. The separate “eddies” drawn in the figure can be considered as all co-existing, or can be considered as a single eddy at various points in time.
In regard to
Figure 9, it is worth noting that a single eddy (or any scatterer) travelling at 30 m/s for a period of 10 s will travel 300 m in that time. At 5 km altitude, this corresponds to an angular change of tan
−1(0.3/5) = 3.5°. So such a scatterer has time to cross from one side of the beam to the other in 10 s. Hence, even a single scatterer will travel from C to D in
Figure 9 during a typical data-acquisition time. If longer acquisition samples of, say, 20–30 s are used, the same is still true: the eddy will exist at different points within the beam during a typical acquisition, and the positions will cover a substantial portion of the beam width. Any spectrum formed using data-lengths of~10–30 s will encompass locations of the eddy (or eddies) covering a relatively large fraction of the beam.
Now consider scatter from the ellipsoids in
Figure 9. Pulses from the transmitter are transmitted radially and will follow trajectories represented by
TA,
TB, and
TC as examples. Each strikes a different eddy (or, if there is only one eddy, the radar paths strike that eddy at different positions as time passes). Due to the alignment of eddy “A”, it reflects most of its energy back to the receiver. But eddies B and C reflect energy off-axis (as shown by the broken arrows) and so the signal received at the radar will be diminished. (While we speak of “reflection”, in reality, the process should be treated as a scattering process, but this simple colloquial discussion is adequate here).
From
Figure 9, scatter will be strongest from eddy “A”, and the more anisotropic the ellipsoids, the more dominant will be the effect of eddy “A”.
Hence, despite the fact that the eddy moves uniformly through the beam, scatter will be dominated by eddy “A” due to its alignment. The radial component of the velocity at this point will be positive (away from the antenna array), and so the Fourier spectrum of the time-series will be dominated by positive frequencies. Hence, the radar analysis will produce a positive velocity, even though there is no vertical motion. Furthermore, the radial velocity “measured” will be proportional to the horizontal wind.
At the current point in time, this model seems to best explain our data, as it gives a natural way for some of the horizontal motions to be converted to apparent vertical motions. Turbulence is a frequent occurrence in the atmosphere, so the radar effects produced by this mechanism can easily persist over the course of months and years, as seen in our results. Not only does the model match our data, but our data allow us to quantify the mean eddy-tilting in patches of turbulence to an accuracy (in principle) of 0.2° and better—a new capability not previously available, giving new insights into the nature of atmospheric turbulence.
Even if turbulence is not involved, tilted quasi-reflectors offer the same simple means of explaining the linear relationship between horizontal and vertical speeds; if a mirror is tilted at an angle
θ∗ to the horizontal orientation and moves horizontally a distance δ
x in time
δt at speed
Ux, then the perpendicular reflection point of the mirror for the vector
TA will move
δxsin
θ∗ radially, so the apparent radial velocity is
δx/δt sin
θ∗ =
Uxsin
θ∗. So the idea of tilted, elongated scatterers/ellipsoids/quasi-reflectors existing with slight tilts is the simplest model to explain the observed correlations. Reference [
44] considered the mathematical treatment of scatter from ellipsoids, and [
45] extended that discussion to different types of scatterers and showed how the ratio of major to minor axis lengths of ellipsoids can be deduced from radar measurements. But if such tilted scatterers are to explain our observations, it still needs to be determined how they are produced, and why they all have similar tilts.
The above discussions have been somewhat qualitative, but we now note that the “tilt angle” we measure will be moderated by the beam itself (see
Figure 9), and the angles shown in
Figure 8 could even be slightly larger in reality.
Figure 10 will now be employed to obtain an estimate for the typical corrections required for the values of
θB shown in
Figure 7 and
Figure 8.
Figure 10a shows an adaptation of figure 7.4 from [
20], which was used to determine a relationship between the radial velocity measured with the tilted off-vertical beam of a radar compared to the true horizontal velocity component along the beam direction. It is shown in [
45] as well as [
20] (and various other references cited within [
20]) that the radial velocity measured is that which would be determined as if the radar beam was aligned at the angle
θeff shown in
Figure 10a rather than the true angle of the beam
θT. The angles
θeff and
θT are related by
This is equation (7.18) from [
20], where
θ0 and
θa are determined as follows. First, the polar diagram of the two-way main beam of the array is assumed to have a form proportional to exp{−
sin2θ/
sin2θ0}. Then,
θ0 represents a radar-related “beam-width” parameter. As discussed in [
20], this means that the two-way half-power half-width of the beam
θ1/2 relates to
θ0 as
θ0 =
θ1/2/√(
ln2). Our values of
θ0 thus vary between 2.0° (Walsingham and McGill), 2.3° (Harrow, Wilberforce, and Eureka) and 2.8° (Negro Creek); see
Appendix A.
In regard to
θa, the back-scattered power is assumed, for simplicity, to have a Gaussian distribution of the form exp{−
sin2θ/
sin2θa}, where
θ is the angle of back-scatter and
θ = 0 corresponds to direct back-scatter (perpendicular to the major axis of the ellipse). Note that [
20] used the symbol
θs instead of
θa; we have used
θa here, as “
θs” has been used for other purposes in this paper. In this case, consider the subscript “
a” to mean “anisotropic”, so that
θa represents the “anisotropy” parameter discussed a few paragraphs above, and can be used to describe either our ellipsoids or the “shards of glass” analogy previously discussed.
Now turn to
Figure 10b. This shows the situation under current consideration. The ellipsoids (or scatterers generally) are pointing slightly downward in the direction of the mean wind, as observed in our data. The radar beam is set to vertical. The wind is shown to come from the right rather than the left, for reasons that will become clear shortly, but the key point is that the eddies slope down and forward in the direction of the mean wind.
This figure is now modified by rotating it clockwise so that the ellipses become horizontal, producing
Figure 10c. The axis A′ in this figure is parallel to the minor axis of the ellipse, and the vertical axis of the atmosphere (i.e., the component parallel to the force of gravity) is now sloping (labelled “vertical”). The figure now looks like
Figure 10a. Hence, whatever mathematics was applied to
Figure 10a in [
20] can now also be applied here, but in the new coordinate system. So we may write
However,
θ′eff is the angle relative to A′, which is, in turn, parallel to the minor axes of the ellipses. We are interested in the angle relative to true (gravitational) vertical, which is labelled
θs in the figure, and is conceptually the same angle as
θB displayed in
Figure 7 and
Figure 8 (i.e., it is the tilt of the major axes of the ellipses relative to horizontal). Clearly,
θ′eff = θp − θs. So, if we assume small angles, it is relatively easy to produce the expression
which can be rewritten as
Hence, the true slope of the scatterers
θP can be found from the measured values in
Figure 7 and
Figure 8, with
θs = θB, provided that
θ0 and
θa are known. It will be seen that in this coordinate system the horizontal wind points up and to the left, but this has no impact on the determination of the effective beam-pointing direction, and the nominal vertical velocity can still be found as the dot-product of the wind vector and a unit vector parallel to the effective beam.
The point needs to be made that this calculation is only a first-order approximation.
Figure 10a–c are not drawn to scale; the angles in the figure are more extreme than in real life. In
Figure 10a, the angle
θT is realistically in the order of 10 to 15 degrees. But in
Figure 10c, the angle
θP is much smaller than is drawn; the actual values are of the order of 1° to 4°, or even less. But in any region of space, there are likely to be multiple ellipsoids, each with different values of
θa. For a near-vertical beam, as in
Figure 10b,c, the dominant scatterers will have small
θa values, but at larger beam-tilts away from the vertical orientation (as in
Figure 10a), the more specular scatterers will not be visible due to their low values of
θa. Thus, for the large beam-tilt case, concentration can be focused on the values with larger
θa. In this case, the scatterers do not vary much across the beam. But in
Figure 10b,c, the situation is better represented by
Figure 9, where the paths to the scatterers (shown by the vectors
TA,
TB, and
TC) have different angles of attack on their respective ellipsoids. A more thorough treatment is then required which recognizes the different weightings relevant for ellipsoids A, B, and C. We will not do that here.
Nevertheless, Equation (7) gives a good first-order approximation for correcting the tilt angle. As an example, representative values of
θa can be found from [
20], figures 7.19, and 7.20a. The figure 7.19 in [
20] suggests a value for
θa of the order of 4° for a vertical beam in the presence of strong anisotropy, while figure 7.20a in [
20] suggests values ranging from 3° to 6° for a very anisotropic tropopause. Reference [
16] presents evidence for values of
θa as small as 1°. If we assume a typical value for
θ0 for the radars of 2.5°, and use a value for
θa of 3°, then from Equation (7),
θP/
θs ≈ 2.5. This may be slightly larger than a full theory would predict, but is suitable as a first guess; so the slopes in
Figure 7 and
Figure 8 should be of the order of 2–3 × larger than those shown in
Figure 7 and
Figure 8.
It is worth considering two other special cases. First, the case that
θa = 0 corresponds to a mirror-like reflector at T
A in
Figure 9, and the term
(θ02 + θa2)/θ02 in Equation (7) gives 1.0, so
θP =
θs, which makes sense. Second, if
θa is very large, then the scatterers are close to isotropic. Strictly, Equation (7) only applies for small angles, but it is still of interest to look at application for the isotropic case. Then,
(θ02 + θa2)/θ02 is also large—it could even be infinite—but, at the same time, isotropic scatter corresponds to the zero slope in
Figure 3a, so
θs(
θ02 + θa2)/
θ02 is zero multiplied by a large number (possibly infinity) and so could be considered to be undefined. In some ways, this is to be expected, since it corresponds to a zero correlation (a condition that we have already determined should occur for isotropic scatter), and hence an unknown slope. So that makes sense too.
We will leave
Figure 7 and
Figure 8 as they are, so they basically show the effective pointing angles of the beams, and readers should recognize that the true tilt angles of the scatterers from horizontal are somewhat greater, with the correction being given by Equation (7) or an equivalent expression. To obtain estimates of the length to depth ratios of the ellipsoids (ratio of major to minor axes), the reader can consult [
45] or [
20] or Equation (7).
5.6. The Importance of Wind Shear
The theory presented by [
43] utilizes a wind jet, but it is possible that similar processes can occur in a more general wind profile which includes a wind shear with increasing altitude. Such additional cases are shown in
Figure 11b. In
Figure 11b, it is envisaged that there exists a wind profile which increases with height, while a spectrum of gravity waves is produced independently lower down. Waves from below therefore move upward as well as horizontally to both the left and right. Waves moving to the right will rise into ever-increasing mean winds until eventually the point is reached where the phase speed of the wave equals the background wind speed. This is called a “critical level”, at which point the wave may break and produce turbulence. On the other hand, waves moving to the left will grow in amplitude, and the point may be reached where the amplitude equals the intrinsic wave speed, giving rise to convective breakdown (e.g., see [
20], equations (11.27)–(11.30)), and also [
46]). Convective breakdown commonly leads to wave breakdown and, therefore, to turbulence. The structures produced may have a preferential tilt bias as they break (as in
Figure 11a), which in turn leads to anisotropic eddies within the turbulence having a tilt bias.
Reference [
47] has produced arguments that suggest that the degree of anisotropy of an eddy depends on the background wind shear
du/
dz. Although they did not discuss the mean orientation of the anisotropic eddies, it seems likely that
du/
dz might also affect the tilt of these entities. For example, if an anisotropic eddy forms pointing downward in the direction of the mean wind, then, in the presence of an increasing vertical wind shear, the tail of the eddy, being higher up and in a region of increased wind speed, will move forward faster than the head, resulting in a rolling motion that steepens the slope of the eddy. If, on the other hand, the eddy was formed with a slight upward tilt parallel to the wind, then the front will move ahead faster than the tail, and the eddy may be stretched and become flatter. So, in both cases, there is a tendency to “roll” the eddy clockwise. It seems likely, then, that the background wind shear plays a role in producing a downward slope to the eddies. This process is indicated in
Figure 12.
Very clear evidence of this possibility comes from [
48]. This paper presents contours of power as a function of angle very close to vertical, using 64 closely spaced near-vertical beams with the MU radar. The results clearly show that the maximum power was frequently not quite vertically overhead, but offset. Indeed, that seemed to be true more often than not. The results are very similar to
Figure 10c, recognizing that true vertical is indicated by the sloping axis labelled “vertical”. Reference [
48] then entered into an extensive discussion about the reasons for this, and concluded that the reason was due to wind-shear rotating the more anisotropic eddies off-vertical. The results of [
48] are also qualitatively consistent with
Figure 9.
Reference [
48] also presents the following quote from [
49] to support their hypothesis of the importance of wind shear: “gravity-wave breaking, being asymmetrical according to the direction of propagation of the waves relative to the mean shear, will modify an existing wave-field of internal waves, and possibly leave a wave-field with directional asymmetry”.
At this stage, the results are interesting, but somewhat speculative. Therefore, it is important to quantitatively ascertain the impact of shears.
Figure 12 helps us do that.
Figure 12 shows that the change in angular tilt
γ of an anisotropic eddy due to a wind shear
du/
dz during a time
δt is
where the variables are defined in
Figure 12. The higher wind speed at greater altitude pushes the upper tail of the eddy forward relative to the lower front end. It is of value to calculate a typical value for
δγ. First, an eddy lifetime is needed. Taking a typical energy dissipation rate
ε at the edge of the turbulent layer (where turbulent dissipation is weakest) as
ε = 10
−4 Wkg
−1 (e.g., see [
20], figure 11.30), and using
ε ≈ L2T−3, and supposing a typical value for
lh of 10 m (the eddy thickness along its minor axis will be of the order of the radar Bragg scale, ~3 m) gives an eddy lifetime of around (100/10
−4)
0.333 ≈ 100 s. Assuming
γ0 = 1°, then
lz/lh ≈ 0.02, and taking a strong but not excessive local wind-shear of 20 ms
−1 km
−1 (0.02 s
−1) gives
δγ = 0.02 × 0.02 × 100 = 0.04 radians, or 2.3°. So an initial tilt angle of 1° is changed to 3.3° during the lifetime of the anisotropic eddy. This is a significant change, and is compatible with our typical tilt angles. So, depending on the stage of the development of the eddy and its initial tilt on formation, it could have any tilt from 1 to 3.5 or more degrees. The turbulent layer will have a mixture of such eddies at various temporal stages of formation and decay.
The discussions in [
48] are therefore extremely supportive of our own data, although the techniques used in their work and ours are entirely different. We consider rotating of the eddies within turbulence via wind shear to be a very strong candidate to explain our observations.