Abstract
Blade antennas are preferred antenna structures for airborne applications due to their compact size, lightweight and drag-reducing aerodynamic shape. In this paper, we present the design, simulation and realization of a miniaturized blade antenna requiring a small ground plane and covering the frequency band 0.8–1.1 GHz. To reduce air drag, the proposed antenna is placed inside an aerodynamically optimized airborne radome. The return loss, the radiation patterns and the realized gain of the proposed antenna are studied using HFSS simulations. The comparison of the simulated return loss and radiation patterns to their measured counterpart demonstrates a good agreement. A minimum realized gain of 3.6 dB was achieved at the frequency of 0.9 GHz.
Sign-in/Register to access full text options 
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 callDisclaimer: 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.
