Abstract
RCS contribution of engine inlet structure to the overall RCS of an aircraft is mainly considered. Using MOM based full-wave numerical analysis method, RCS of target aircraft model is calculated for frequency and direction(horizontal, vertical angle) in monostatic condition. Related to the frequency characteristics of the engine inlet structure, RCS enhancements in front angular region can be seen at the specific frequency region.
Original language | English |
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Title of host publication | 2018 IEEE Antennas and Propagation Society International Symposium and USNC/URSI National Radio Science Meeting, APSURSI 2018 - Proceedings |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 2335-2336 |
Number of pages | 2 |
ISBN (Electronic) | 9781538671023 |
DOIs | |
Publication status | Published - 2018 |
Event | 2018 IEEE Antennas and Propagation Society International Symposium and USNC/URSI National Radio Science Meeting, APSURSI 2018 - Boston, United States Duration: 2018 Jul 8 → 2018 Jul 13 |
Publication series
Name | 2018 IEEE Antennas and Propagation Society International Symposium and USNC/URSI National Radio Science Meeting, APSURSI 2018 - Proceedings |
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Conference
Conference | 2018 IEEE Antennas and Propagation Society International Symposium and USNC/URSI National Radio Science Meeting, APSURSI 2018 |
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Country/Territory | United States |
City | Boston |
Period | 18/7/8 → 18/7/13 |
Bibliographical note
Funding Information:ACKNOWLEDGMENT This research was carried out as part of the ”Very High Frequency Radar Technology for Stealth Target Detection” task of the Agency for Defense Development.
Publisher Copyright:
© 2018 IEEE.
All Science Journal Classification (ASJC) codes
- Computer Networks and Communications
- Instrumentation
- Radiation