Investigation of field coupling into a carbon fiber aircraft fuselage with the method of moments

Start Page
311
End Page
314
Article Number
6046360
Citation
Proceedings - 2011 International Conference on Electromagnetics in Advanced Applications, ICEAA'11 (): 6046360 311-314 (2011)
Contribution to Conference
13th International Conference on Electromagnetics in Advanced Applications, ICEAA 2011 
Publisher DOI
10.1109/ICEAA.2011.6046360
Scopus ID
2-s2.0-80155137066
Publisher
IEEE
In this paper the field coupling into a fuselage model consisting of carbon fiber composite with apertures is analyzed by means of the Method of Moments. A set of two boundary integral equations, involving two current layers, is applied for accurate treatment of aperture coupling. The considered anisotropic shell is investigated by two approaches, where the modeling is accomplished using boundary impedances and a multilayer technique, respectively. The applicability of these techniques is studied and validated by reference computations on generic test objects. It turns out that the results gained by the proposed techniques are in very good agreement with results of the finite element method. © 2011 IEEE.
DDC Class
600: Technik
620: Ingenieurwissenschaften