{"title":"飞机大小混响室和搅拌器的设计、建造、计算电磁建模和表征","authors":"K. Goldsmith, P. A. Johnson","doi":"10.1109/DASC.1998.741554","DOIUrl":null,"url":null,"abstract":"The Defence Science and Technology Organisation has conducted a research program to investigate the performance of reverberation chambers in establishing military aircraft electromagnetic vulnerability (EMV). The construction of an aircraft-sized chamber for research purposes offers special challenges, mostly financial. The most critical design parameters are the chamber dimensions, mode tuner size and wall material.","PeriodicalId":335827,"journal":{"name":"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1998-10-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":"{\"title\":\"Design, construction, computational EM modelling, and characterisation of an aircraft sized reverberation chamber and stirrer\",\"authors\":\"K. Goldsmith, P. A. Johnson\",\"doi\":\"10.1109/DASC.1998.741554\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The Defence Science and Technology Organisation has conducted a research program to investigate the performance of reverberation chambers in establishing military aircraft electromagnetic vulnerability (EMV). The construction of an aircraft-sized chamber for research purposes offers special challenges, mostly financial. The most critical design parameters are the chamber dimensions, mode tuner size and wall material.\",\"PeriodicalId\":335827,\"journal\":{\"name\":\"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)\",\"volume\":\"9 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1998-10-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"6\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/DASC.1998.741554\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC.1998.741554","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Design, construction, computational EM modelling, and characterisation of an aircraft sized reverberation chamber and stirrer
The Defence Science and Technology Organisation has conducted a research program to investigate the performance of reverberation chambers in establishing military aircraft electromagnetic vulnerability (EMV). The construction of an aircraft-sized chamber for research purposes offers special challenges, mostly financial. The most critical design parameters are the chamber dimensions, mode tuner size and wall material.
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