Lightning and electro-magnetic pluse-induced fuselage skin currents can magnetically or electrically flux couple onto air-craft cabling through dielectric "holes" or apertures in the aircraft fuselage. Using lightning transient analysis (LTA) input-output waveform records, frequency domain techniques are presented that locate the exact point of excitation. The techniques are demonstrated using an RG-58 cable simulation and are then applied to the yaw damper circuit of a USAF F-111.


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    Title :

    Identification of Voltage Transients on Aircraft Cabling under LTA Excitation


    Contributors:

    Published in:

    Publication date :

    1979-05-01


    Size :

    2018140 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English