Figure 6
From: Z-folding aircraft electromagnetic scattering analysis based on hybrid grid matrix transformation
RCS of the outer wing 1 under different radar wave frequencies, β = 0°, ωr1 = 0.3142 rad/s.
Figure 6 | Scientific Reports
From: Z-folding aircraft electromagnetic scattering analysis based on hybrid grid matrix transformation
RCS of the outer wing 1 under different radar wave frequencies, β = 0°, ωr1 = 0.3142 rad/s.
