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

Access to Document

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: [email protected]). 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: [email protected]). Digital Object Identifier 10.1109/TEMC.2005.851729

PY - 2005/8

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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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UR - https://www.scopus.com/pages/publications/27644463442#tab=citedBy

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DO - 10.1109/TEMC.2005.851729

M3 - Article

SN - 0018-9375

VL - 47

SP - 667

EP - 670

JO - IEEE Transactions on Electromagnetic Compatibility

JF - IEEE Transactions on Electromagnetic Compatibility

IS - 3

ER -

HIRF penetration into simplified fuselage using a reverberation chamber approach

Abstract

Keywords

ASJC Scopus subject areas

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