This is an EMCC benchmark target referenced in:
The Efield MLFMM was used to compute the RCS of the almond. Two different length of the almond was used in the simulations. Two different material cases was studied, a PEC case and a coated case.
Two different geometrical configurations was used in the simulation of RCS. The definition of the geometry is shown in Figure 2.
Figure 1: The NASA almond |
Figure 2: Definition of geometry of NASA almond |
In Figure 3 and Figure 4 the monostatic RCS are shown and compared with measurement results. In Figure 5 the surface currents are shown.
Figure 3: Monostatic RCS of 9 inch PEC NASA almond at 7 GHz in azimuth plane. Polarization VV. Computations (left) and results from Alex C. Woo, Helen T. G. Wang, Michael J. Schuh, and Michael L. Sanders (right). |
Figure 4: Monostatic RCS of 9 inch PEC NASA almond at 7 GHz in azimuth plane. Polarization HH. Computations (left) and results from Alex C. Woo, Helen T. G. Wang, Michael J. Schuh, and Michael L. Sanders (right). |
Figure 5: Surface currents of 9 inch PEC NASA almond at 7 GHz |
In Figure 6 the monostatic RCS is shown.
Figure 6: Monostatic RCS of 9 inch coated NASA almond at 3 GHz in upper x-z plane. In black pure PEC case, in red coated case with εr =1, μr =1 and CFIE, in blue coated case with εr =1, μr =1 and EFIE, in green coated case with εr =3-2i, μr =2-i and CFIE and in magenta coated case with εr =3-2i, μr =2-i and EFIE. |
In Figure 7 the bistatic RCS is shown and in Figure 8 the surface currents is shown.
Figure 7: Bistatic RCS of 2.5m PEC NASA almond at 8 GHz in x-y-plane (left) and x-z-plane (right). |
Figure 8: Surface currents of 2.5m PEC NASA almond at 8 GHz |
In Figure 9 the bistatic RCS is shown.
Figure 9: Bistatic RCS of 2.5m coated NASA almond at 1 GHz in x-y-plane. |