DocumentCode :
357880
Title :
The design of an internal current strike demonstrator
Author :
Burnham, A. ; Nelson, R. ; Glower, J. ; Jorgenson, J. ; Heizelman, D. ; Heather, F.
Author_Institution :
BF Goodrich Aircraft Sensors Div., Burnsville, MN, USA
Volume :
1
fYear :
2000
fDate :
2000
Firstpage :
415
Abstract :
When lightning strikes an airplane, it generally attaches to a leading edge such as a wing tip and leaves via a sharp trailing edge such as the rear wing tip or tail. Lightning currents now from the point of attachment to the point of exit, the actual path of which is a function of the aircraft surface conductivity. If the aircraft surfaces are poorly conducting, current paths may inadvertently go through aircraft fuel tanks-which may result in a fuel tank explosion. In order to clearly visualize this phenomena, an internal current strike demonstrator was designed and constructed by students at North Dakota State University for the Naval Air Warfare Center Aircraft Division. This paper describes the design and development of the demonstrator
Keywords :
aircraft testing; electric current; electromagnetic induction; lightning; surface conductivity; EM induction; Naval Air Warfare Center Aircraft Division; North Dakota State University; aircraft surface conductivity; airplane; current paths; fuel tank explosion; internal current strike demonstrator; leading edge; lightning currents; rear wing tip; sharp trailing edge; tail; wing tip; Circuits; Conducting materials; Conductivity; Electrochemical processes; Explosions; Fuel storage; Level control; Lightning; Piezoelectric devices; Sparks;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electromagnetic Compatibility, 2000. IEEE International Symposium on
Conference_Location :
Washington, DC
Print_ISBN :
0-7803-5677-2
Type :
conf
DOI :
10.1109/ISEMC.2000.875604
Filename :
875604
Link To Document :
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