J
J. Fisher
Researcher at Papua New Guinea University of Technology
Publications - 11
Citations - 33
J. Fisher is an academic researcher from Papua New Guinea University of Technology. The author has contributed to research in topics: Lightning & Lightning strike. The author has an hindex of 2, co-authored 9 publications receiving 11 citations.
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Journal ArticleDOI
Applying a 3D Dipole Model for Lightning Electrodynamics of Low-Flying Aircraft
TL;DR: In this paper, a detailed electrostatic model of an aircraft was used in an experimentally validated, new electric-charge-based circuit model for studying aircraft-lightning electrodynamics.
Proceedings ArticleDOI
Cloud to Ground and Ground to Cloud Flashes in Lightnin g Protection: And Future Severe Lightnin g and Climate Change
TL;DR: In this paper, the authors report on the direct effect of lightning strike on an aircraft when subject to both ground to cloud (GC) and cloud to ground (CG) flashes and compare the parameters of both types of earth flashes.
Proceedings ArticleDOI
Intelligent localisation of signals using the signal wavefronts: A review
TL;DR: A model to correctly represent both lighting return stroke currents and the radiated lightning electromagnetic pulses is presented with carefully chosen damping coefficients, or frequencies, following a previous work on this.
Journal ArticleDOI
Pre-Lightning Strikes and Aircraft Electrostatics
TL;DR: In this article, the authors applied the 3D dipole model in predicting the electrostatics build up along an aircraft extremities as it approached an ambient electric field of a charged cloud.
Proceedings ArticleDOI
Three dimensional electric dipole model for lightning-aircraft electrodynamics and its application to low flying aircraft
TL;DR: In this paper, a new electric charge based circuit model for studying aircraft-lightning electrodynamics and its application to an aircraft taking off or landing is presented, which is used to characterize the electrical currents and electric potential fluctuations on an aircraft to determine alternative design approaches to minimize the severity of the aircraft dynamics.