HIRF virtual testing on C-295 aircraft validated with FSV method
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Fernández Pantoja, Mario Alberto; Gutierrez Gutierrez, Guadalupe; Alvarez Gonzalez, Jesús; Pascual Gil, Enrique; Bandinelli, Mauro; Guidi, Rodolfo; Martorelli, Valerio; González García, SalvadorMateria
Electromagnetic Electromagnetic compatibility Feature selective validation Finite difference time domain High-intensity radiated fields Low-level swept fields Oversized cavity theory Perfect electric conductor Radio frequency Time domain analysis
Fecha
2014Referencia bibliográfica
Fernandez Pantoja, Mario; et. al. HIRF virtual testing on C-295 aircraft validated with FSV method. IEEE Transaction on Electromagnetic Compatibility, vol.56, no.4, pp. 854,863, 2014 [http://hdl.handle.net/10481/50134]
Patrocinador
This work was supported by the funding from the European Com- munity Seventh Framework Programme FP7/2007-2013, under Grant 205294 (HIRF SE project), from the Spanish National Projects TEC2010-20841-C04- 04, CSD2008-00068, from the Junta de Andalucia Project P09-TIC-5327, and from the Granada Excellence Network of Innovation Laboratories (GENIL) projectResumen
In this paper, we show the application of numerical
simulation for the virtual testing of a very complex system under
high-intensity radiated fields (HIRF) conditions. Numerical results
have been compared to measurements performed on a C-295 air-
craft. The approach is based on the use of multiple tools for the
preprocessing, computation, and postprocessing, all of them in-
tegrated under the same framework. This study is a part of the
HIRF SE project, and the final step for the validation of the tools
involved there, to introduce the use of simulation in the whole air-
craft certification process in an HIRF environment. The main goal
of the project is to provide the aeronautic industry with a numerical
modeling computing framework, which could be used to predict
the electromagnetic performance, and to carry out parametrical
studies during the design phase, when changes are simpler and less
costly. It could also lead in the future to a considerable reduction on
the certification/qualification testing phase on air vehicles, to cross
validate the results obtained from measurement and simulation
providing best confidence in them, and to attain a more exhaustive
analysis to achieve a higher level in the air vehicle safet