DocumentCode
332569
Title
Design, construction, computational EM modelling, and characterisation of an aircraft sized reverberation chamber and stirrer
Author
Goldsmith, Kevin R. ; Johnson, Paul A.
Author_Institution
Defence Sci. & Technol. Organ., Salisbury, SA, Australia
Volume
1
fYear
1998
fDate
31 Oct-7 Nov 1998
Abstract
The Defence Science and Technology Organisation has conducted a research program to investigate the performance of reverberation chambers in establishing military aircraft electromagnetic vulnerability (EMV). The construction of an aircraft-sized chamber for research purposes offers special challenges, mostly financial. The most critical design parameters are the chamber dimensions, mode tuner size and wall material
Keywords
aerospace test facilities; electromagnetic interference; military aircraft; reverberation chambers; aircraft sized reverberation chamber; chamber dimensions; computational EM modelling; electromagnetic vulnerability; military aircraft; mode tuner size; stirrer; wall material; Aerospace electronics; Aircraft manufacture; Aircraft propulsion; Anechoic chambers; Australia; Computational modeling; Costs; Military aircraft; Reverberation chamber; Tuners;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location
Bellevue, WA
Print_ISBN
0-7803-5086-3
Type
conf
DOI
10.1109/DASC.1998.741554
Filename
741554
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