HIRF Transfer Functions of a Fuselage Model: Measurements and Simulations

An entire set of high-intensity radiated field transfer functions including the main types of contemporary test methods is presented. Consequently, the applied frequency range for this task expands over many decades, from the kilohertz range up to 40 GHz. A major aim is to demonstrate the applicatio...

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Veröffentlicht in:	IEEE transactions on electromagnetic compatibility 2014-04, Vol.56 (2), p.311-319
Hauptverfasser:	Rasek, Guido A., Pascual-Gil, Enrique, Schroder, Arne, Junqua, Isabelle, Guidi, Rodolfo, Kreller, Christian A., Bruns, Heinz-Dietrich, Loos, Steffen E.
Format:	Artikel
Sprache:	eng
Schlagworte:	Airframes Asymptotic Atmospheric modeling Classical and quantum physics: mechanics and fields computational electromagnetics (CEM) Computational modeling Computer simulation Conductors direct current injection (DCI) Electromagnetic compatibility Exact sciences and technology finite-difference time domain (FDTD) Foundations, theory of measurement, miscellaneous theories (including aharonov-bohm effect, bell inequalities, berry's phase) Fuselages high-intensity radiated fields (HIRF) Impedance low-level direct drive (LLDD) low-level swept current (LLSC) low-level swept field (LLSF) Mass and density Mathematical models Measurement and error theory Measurements common to several branches of physics and astronomy method of moments (MoM) Metrology Metrology, measurements and laboratory procedures Numerical models Physics power balance (PWB) Quantum mechanics Resistors Solvers Spatial dimensions (e.g.: position, lengths, volume, angles, displacements, including nanometer-scale displacements) Tasks Transfer functions
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Beschreibung
Zusammenfassung:	An entire set of high-intensity radiated field transfer functions including the main types of contemporary test methods is presented. Consequently, the applied frequency range for this task expands over many decades, from the kilohertz range up to 40 GHz. A major aim is to demonstrate the application of numerical computer modeling for such a task. Results of measurements and various solvers are compared to each other. As the activity serves also for the validation of such applications, the scenario is investigated by the use of a fuselage model with limited complexity.
ISSN:	0018-9375 1558-187X
DOI:	10.1109/TEMC.2013.2287049