DocumentCode
1731522
Title
Application of numerical analysis to the electromagnetic effects validation of aircraft
Author
Perala, R.A. ; Rudolph, T.H. ; McKenna, P.M. ; Jones, Chris
Author_Institution
Electro Magnetic Applications, Denver, CO, USA
fYear
1993
Firstpage
185
Lastpage
190
Abstract
The authors present the capabilities of the time-domain three-dimensional finite difference method EMA3D for the solution of Maxwell´s equations. They describe the method and then give six examples of comparison of numerical results with test data. The examples are NASA F-106B in-flight natural lightning external response, USAF/FAA CV-580 in-flight natural lightning external response, NASA F-106B in-flight natural lightning internal cable response, NASA F-106B self-consistent nonlinear triggered lightning response, SAAB JAS39 lightning response of carbon fiber wing box, and SAAB JAS39 lightning validation test. The EMA3D method has been shown to be able to solve a wide variety of problems involving complex geometries, complex sources, and complex materials
Keywords
aircraft; electromagnetic compatibility; finite difference methods; lightning protection; EMA3D method; EMI; Maxwell´s equations; NASA F-106B; SAAB JAS39; USAF/FAA CV-580; carbon fiber wing box; civil transport aircraft; complex geometries; complex materials; electromagnetic effects validation; helicopter; in-flight natural lightning response; lightning validation test; nonlinear triggered lightning response; numerical analysis; numerical results; time-domain three-dimensional finite difference method; Automatic testing; FAA; Finite difference methods; Lightning; Maxwell equations; NASA; Numerical analysis; Optical fiber cables; Optical fiber testing; Time domain analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1993. 12th DASC., AIAA/IEEE
Conference_Location
Fort Worth, TX
Print_ISBN
0-7803-1343-7
Type
conf
DOI
10.1109/DASC.1993.283549
Filename
283549
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