Statistics of EM field inside a scale model fuselage using a reverberation chamber approach

Anastasios H. Panaretos; Craig R. Birtcher; Constantine Balanis

Statistics of EM field inside a scale model fuselage using a reverberation chamber approach

Anastasios H. Panaretos, Craig R. Birtcher, Constantine Balanis

IAFSE-ECEE: Electrical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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
State	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

ASJC Scopus subject areas

Electrical and Electronic Engineering

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Panaretos, AH, Birtcher, CR & 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, 2003 IEEE International Antennas and Propagation Symposium and USNC/CNC/URSI North American Radio Science Meeting, Columbus, OH, United States, 6/22/03.

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title = "Statistics of EM field inside a scale model fuselage using a reverberation chamber approach",

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.",

author = "Panaretos, {Anastasios H.} and Birtcher, {Craig R.} and Constantine Balanis",

year = "2003",

language = "English (US)",

volume = "2",

pages = "1189--1192",

booktitle = "IEEE Antennas and Propagation Society, AP-S International Symposium (Digest)",

note = "2003 IEEE International Antennas and Propagation Symposium and USNC/CNC/URSI North American Radio Science Meeting ; Conference date: 22-06-2003 Through 27-06-2003",

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AU - Panaretos, Anastasios H.

AU - Birtcher, Craig R.

AU - Balanis, Constantine

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Y1 - 2003

N2 - 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.

AB - 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.

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Y2 - 22 June 2003 through 27 June 2003

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