Abstract
The SE of a simplified fuselage was examined using a reverberation chamber approach. Measurements were performed for various mode-stirrer positions and the field distribution at each location was shown to be characterized by the same statistics. This approach resulted in significantly higher field intensities inside the cavity and, thus, lower SE levels compared to the purely deterministic approach. In addition, measured data demonstrate the ability to predict the maximum field inside the fuselage.
| Original language | English (US) |
|---|---|
| Title of host publication | IEEE Antennas and Propagation Society, AP-S International Symposium (Digest) |
| Pages | 1189-1192 |
| Number of pages | 4 |
| Volume | 2 |
| Publication status | Published - 2003 |
| Event | 2003 IEEE International Antennas and Propagation Symposium and USNC/CNC/URSI North American Radio Science Meeting - Columbus, OH, United States Duration: Jun 22 2003 → Jun 27 2003 |
Other
| Other | 2003 IEEE International Antennas and Propagation Symposium and USNC/CNC/URSI North American Radio Science Meeting |
|---|---|
| Country | United States |
| City | Columbus, OH |
| Period | 6/22/03 → 6/27/03 |
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ASJC Scopus subject areas
- Electrical and Electronic Engineering
Cite this
Panaretos, A. H., Birtcher, C. R., & Balanis, C. (2003). Statistics of EM field inside a scale model fuselage using a reverberation chamber approach. In IEEE Antennas and Propagation Society, AP-S International Symposium (Digest) (Vol. 2, pp. 1189-1192)