HIRF penetration into simplified fuselage using a reverberation chamber approach

Tassos Panaretos; Constantine Balanis; Craig R. Birtcher

doi:10.1109/TEMC.2005.851729

HIRF penetration into simplified fuselage using a reverberation chamber approach

Tassos Panaretos, Constantine Balanis, Craig R. Birtcher

Electrical Engineering

Research output: Contribution to journal › Article › peer-review

10 Scopus citations

Abstract

In this paper, hightintensity radiated fields (HIRF) penetration into aircraft fuselage is studied using a reverberation chamber approach. A mode-stirrer is constructed and placed inside a simplified scale fuselage model. Measurements of the penetrating field are performed for different mode-stirrer positions. The collected sets of data are statistically processed and their probability distributions are investigated. Goodness-of-fit tests are performed between data empirical cumulative density functions and existing theoretical probability models which govern the electromagnetic field variations inside reverberation chambers.

Original language	English (US)
Pages (from-to)	667-670
Number of pages	4
Journal	IEEE Transactions on Electromagnetic Compatibility
Volume	47
Issue number	3
DOIs	https://doi.org/10.1109/TEMC.2005.851729
State	Published - Aug 2005

Keywords

Cumulative density function
High-intensity radiated fields (HIRF)
Mode stirrer
Reverberation chamber
Simplified fuselage

ASJC Scopus subject areas

Atomic and Molecular Physics, and Optics
Condensed Matter Physics
Electrical and Electronic Engineering

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10.1109/TEMC.2005.851729

Cite this

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title = "HIRF penetration into simplified fuselage using a reverberation chamber approach",

abstract = "In this paper, hightintensity radiated fields (HIRF) penetration into aircraft fuselage is studied using a reverberation chamber approach. A mode-stirrer is constructed and placed inside a simplified scale fuselage model. Measurements of the penetrating field are performed for different mode-stirrer positions. The collected sets of data are statistically processed and their probability distributions are investigated. Goodness-of-fit tests are performed between data empirical cumulative density functions and existing theoretical probability models which govern the electromagnetic field variations inside reverberation chambers.",

keywords = "Cumulative density function, High-intensity radiated fields (HIRF), Mode stirrer, Reverberation chamber, Simplified fuselage",

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

note = "Funding Information: Manuscript received April 6, 2004; revised January 10, 2005. This work was supported by the National Aeronautics and Space Administration under Grant NAG-1-1781 and Cooperative Agreement NCC-1-01051. The authors are with the Department of Electrical Engineering, Arizona State University, Tempe, AZ 85287-5706 USA (e-mail: balanis@asu.edu). Digital Object Identifier 10.1109/TEMC.2005.851729",

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AU - Panaretos, Tassos

AU - Balanis, Constantine

AU - Birtcher, Craig R.

N1 - Funding Information: Manuscript received April 6, 2004; revised January 10, 2005. This work was supported by the National Aeronautics and Space Administration under Grant NAG-1-1781 and Cooperative Agreement NCC-1-01051. The authors are with the Department of Electrical Engineering, Arizona State University, Tempe, AZ 85287-5706 USA (e-mail: balanis@asu.edu). Digital Object Identifier 10.1109/TEMC.2005.851729

PY - 2005/8

Y1 - 2005/8

N2 - In this paper, hightintensity radiated fields (HIRF) penetration into aircraft fuselage is studied using a reverberation chamber approach. A mode-stirrer is constructed and placed inside a simplified scale fuselage model. Measurements of the penetrating field are performed for different mode-stirrer positions. The collected sets of data are statistically processed and their probability distributions are investigated. Goodness-of-fit tests are performed between data empirical cumulative density functions and existing theoretical probability models which govern the electromagnetic field variations inside reverberation chambers.

AB - In this paper, hightintensity radiated fields (HIRF) penetration into aircraft fuselage is studied using a reverberation chamber approach. A mode-stirrer is constructed and placed inside a simplified scale fuselage model. Measurements of the penetrating field are performed for different mode-stirrer positions. The collected sets of data are statistically processed and their probability distributions are investigated. Goodness-of-fit tests are performed between data empirical cumulative density functions and existing theoretical probability models which govern the electromagnetic field variations inside reverberation chambers.

KW - Cumulative density function

KW - High-intensity radiated fields (HIRF)

KW - Mode stirrer

KW - Reverberation chamber

KW - Simplified fuselage

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IS - 3

ER -

HIRF penetration into simplified fuselage using a reverberation chamber approach

Abstract

Keywords

ASJC Scopus subject areas

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