Table 3 RCS indicator of outer wing 1, α = 60°, β = 0°, ωr1 = 0.3142 rad/s, t = 0 ~ 3.857 s.

From: Z-folding aircraft electromagnetic scattering analysis based on hybrid grid matrix transformation

fRH (GHz)

2

4

6

8

10

12

Mean (dBm2)

5.5538

6.6450

5.4119

4.4112

2.0405

-0.4535

Peak (dBm2)

22.8069

25.8010

25.7755

24.1351

21.4936

17.5069

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