| Application Project: Radar Cross-Section of Aircraft
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Objective: In this article, we explore computing RCS of electrically large structures, like aircraft.
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Concepts/Features:
- Radar Cross Section
- Large Projects
- Cloud-Based Resources
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Minimum Version Required: All versions
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' Download Link: None
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Introduction
In this article, we compute the bistatic radar cross-section (RCS) of a Dassault Mirage III type fighter aircraft at 850 MHz with EM.Tempo. At 850 MHz, considerable computational resources are required to compute a full-wave result with EM.Tempo's FDTD solver.
Computational Environment
The Mirage III has approximate dimensions (length,wingspan,height) of 15m x 8m x 4.5m. Or, measured in terms of freespace wavelength at 850 MHz, 42.5 lambda x 22.66 lambda x 12.75 lambda. Thus, for the purposes of EM.Tempo, we need to solve a region of about 12,279 cubic wavelengths. For problems of this magnitude, a great deal of CPU memory is needed, and a high-performance CPU is desirable to reduce simulation time.
CAD Model
Project Setup
Results
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Figure 1: Geometry of the periodic unit cell of the dispersive water slab in EM.Tempo.
Last modified on 7 October 2016, at 20:09
