Table 2.
Spread of 
, shown for different viewing angles.
| Case | (θ, ϕ) |
 |
ℒlobe/ℒwing |
|---|---|---|---|
| 3Dmaj_ref | 70° , 0° | −0.294 | 1.5 |
| 20° , 70° | −0.200 | 1.9 | |
| 45° , 45° | +0.092 | 1.4 | |
| 70° , 45° | +0.156 | 1.1 | |
| 3Dang_ref | 70° , 0° | −0.562 | 2.0 |
| 20° , 70° | −0.068 | 2.2 | |
| 45° , 45° | −0.162 | 1.9 | |
| 70° , 45° | −0.065 | 1.5 | |
Notes. This table shows the 
values (Col. 3) that are obtained for frequencies 240 MHz and 610 MHz for our 3D cases (Col. 1), for the four line-of-sight angles as mentioned in Col. 2. The fourth column represents the projected lobe to wing length ratios for each case. A distribution of 
values both in the +ve and −ve sides is particularly noticeable here, which is obtained based on the back-flow model.
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