Parametric Simulation on Reduction of $S$ -Band Rear Bistatic Radar Cross Section of Jet Engine With Vector Thrust Nozzle via Plasmatized Exhaust
-
Published:2017-03
Issue:3
Volume:45
Page:388-404
-
ISSN:0093-3813
-
Container-title:IEEE Transactions on Plasma Science
-
language:
-
Short-container-title:IEEE Trans. Plasma Sci.
Funder
National Science Consul of Taiwan
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Condensed Matter Physics,Nuclear and High Energy Physics