@misc{10481/50287, year = {2017}, url = {http://hdl.handle.net/10481/50287}, abstract = {The increased use of carbon-fiber composites in unmanned aerial vehicles is a challenge for their EMC assessment by numerical solvers. For accurate and reliable simulations, numerical procedures should be tested not only for individual com- ponents, but also within the framework of complete systems. With this aim, this paper presents a benchmark test case based on experimental measurements coming from direct-current injection tests in the SIVA unmanned air vehicle, reproduced by a numerical finite-difference-time-domain solver that employs a new subgrid- ding scheme to treat lossy composite thin panels. Validation was undertaken by applying the feature selective validation method, which quantifies the agreement between experimental and numerical data.}, organization = {This work was supported by the Projects TEC2013-48414- C3- { 1,2,3 } -R, TEC2016-79214-C3- { 1,2,3 } -R, and TEC2015-68766-REDC (Spanish MINECO, EU FEDER), P12-TIC-1442 (J. de Andalucia, Spain), Alhambra-UGRFDTD (AIRBUS DS), and by the CSIRC alhambra.ugr.es supercomputing center.}, keywords = {Aerospace simulation}, keywords = {Finite-difference methods}, keywords = {Numerical analysis}, keywords = {Software verification and validation}, title = {SIVA: A benchmark for numerical validation of composite UAV modeling}, doi = {10.1109/TEMC.2017.2648507}, author = {Ruiz Cabello, Miguel and González García, Salvador and Pous, Marc and Pascual Gil, Enrique and Díaz Angulo, Luis Manuel and López, Patricia and Riu, Pere J. and Mateos, Daniel and Poyatos, David and Fernández, Mireya and Álvarez, Jesús and Gutiérrez, Guadalupe G. and Fernández Pantoja, Mario Alberto and Añón, Manuel and Silva, Ferrán and Rubio Bretones, Amelia Consuelo and Trallero, Rafael and Nuño, Luis and Escot, David and Gómez Martín, Rafael Antonio}, }