Abstract
The penetration of High Intensity Radiated Fields (HIRF) into the fuselage of a Boeing 757-200 is calculated using the Finite-Difference Time-Domain method. The FDTD predictions will eventually be compared with in-flight measurements as part of the validation phase of a study into all-electronic commercial aircraft technology. Ultimately, avionic systems and components would be tested in the lab under the illumination levels predicted to exist at the systems' installed locations in the aircraft. This is in contrast to expensive and hazardous full-aircraft testing.
Original language | English (US) |
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Title of host publication | IEEE International Symposium on Electromagnetic Compatibility |
Editors | Anon |
Publisher | IEEE |
Pages | 670-672 |
Number of pages | 3 |
Volume | 2 |
State | Published - 1998 |
Event | Proceedings of the 1998 IEEE International Symposium on Electromagnetic Compatibility. Part 1 (of 2) - Denver, CO, USA Duration: Aug 24 1998 → Aug 28 1998 |
Other
Other | Proceedings of the 1998 IEEE International Symposium on Electromagnetic Compatibility. Part 1 (of 2) |
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City | Denver, CO, USA |
Period | 8/24/98 → 8/28/98 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering
- Condensed Matter Physics