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 framewo...
The real scale simulator is described which was designed by the Centre d'Etudes de Gramat (CEG) to s...
A high-fidelity HF channel simulation has been developed that is suitable for Over-the-Horizon Radar...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...
Abstract—Preparing the 3D-geometry models to perform electromag-netic compatibility (EMC) numerical ...
The FP7 European project HIRF-SE gathers 44 partners from 11 countries, with a challenging goal: the...
During their missions, helicopters may fly near to high power radar and radio transmitters. These em...
International audienceThis paper describes the 3D FDTD model of an aircraft developed to compute the...
Au cours de leurs missions, les hélicoptères sont susceptibles de voler à proximité d’émetteurs radi...
A crucial issue in the development process of a modern jet transport aircraft is the comprehensive e...
The aim of this work is to explore means to improve the speed of the computational electromagnetics ...
In 1995, the NASA Langley Research Center conducted a series of aircraft tests aimed at characterizi...
The high intensity radiated fields (HIRF) certification process as currently implemented is comprise...
This paper analyzes the influence of simplifications in electromagnetic models used in thedesign of...
The paper presents a time-domain finite-element solver developed for simulations related to solving ...
During the third quarter of 1996, the Closed-Loop Systems Laboratory was established at the NASA Lan...
The real scale simulator is described which was designed by the Centre d'Etudes de Gramat (CEG) to s...
A high-fidelity HF channel simulation has been developed that is suitable for Over-the-Horizon Radar...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...
Abstract—Preparing the 3D-geometry models to perform electromag-netic compatibility (EMC) numerical ...
The FP7 European project HIRF-SE gathers 44 partners from 11 countries, with a challenging goal: the...
During their missions, helicopters may fly near to high power radar and radio transmitters. These em...
International audienceThis paper describes the 3D FDTD model of an aircraft developed to compute the...
Au cours de leurs missions, les hélicoptères sont susceptibles de voler à proximité d’émetteurs radi...
A crucial issue in the development process of a modern jet transport aircraft is the comprehensive e...
The aim of this work is to explore means to improve the speed of the computational electromagnetics ...
In 1995, the NASA Langley Research Center conducted a series of aircraft tests aimed at characterizi...
The high intensity radiated fields (HIRF) certification process as currently implemented is comprise...
This paper analyzes the influence of simplifications in electromagnetic models used in thedesign of...
The paper presents a time-domain finite-element solver developed for simulations related to solving ...
During the third quarter of 1996, the Closed-Loop Systems Laboratory was established at the NASA Lan...
The real scale simulator is described which was designed by the Centre d'Etudes de Gramat (CEG) to s...
A high-fidelity HF channel simulation has been developed that is suitable for Over-the-Horizon Radar...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...