Numerical Analysis of the Lightning on Small Aircraft
This paper deals with numerical analysis of lightning stroke effects on aircraft. Computations are implemented by the use of the time-domain solver (FIT). Attention is turned to a simple model of a composite nose part of the airplane EV-55. The analysis of the model itself is performed for two fundamentally different basic conceptions of a possible protection against direct effects of lightning.
KeywordsNumerical analysis, electromagnetic compatibility, (in)direct effects of lightning, lightning, aircraft
Document typePeer reviewed
Document versionxmlui.vut.verze.Publishers's version
SourceProceedings of the 22nd Conference STUDENT EEICT 2016. s. 333-337. ISBN 978-80-214-5350-0
- Student EEICT 2016