Abstract

In this paper, the shielding effectiveness of a cylindrical scaled fuselage model is examined. Measurements of the penetrated field, are performed as a function of frequency. The penetrated field is further statistically analyzed and its distribution is investigated. For the purposes of this investigation, different probability models are introduced while their ability is tested to match the measured data distribution.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.