A scale model of the Transall C160 military aircraft, 1/10 of the actual, was installed above a large copper ground plate and connected to it. The entry point at the nose was hard-wire connected to a 12- mu F/5-kV capacitor bank, and the current pulse launch was made using a triggered atmospheric-pressure spark gap. The exit point at the tail or at the left wing tip, depending on the configuration, was connected to the ground plate via an 80- Omega waveshaping resistor. The transient electromagnetic fields on the outer skin of the model were measured using D-dot and B-dot sensors. Three D-dot sensors were mounted on the forward upper fuselage, on the top and the bottom of the left wing. Two B-dot sensors were mounted on the forward upper fuselage and on the top of the left wing. The current was also measured using three i-dot sensors mounted on the nose boom, on the left wing tip, and on the tail boom. A comparison of experimental and computed electromagnetic fields on the scale model was performed for two experimental configurations of current injection: nose to tail and nose to left wing. As shown for one typical case, all the data were predicted with excellent frequency agreement and very good amplitude agreement.


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    Title :

    Comparison of experimental and numerical results for transient electromagnetic fields induced on a scale model aircraft by current-injection technique


    Additional title:

    Vergleich der experimentellen und numerischen Ergebnisse von transienten elektromagnetischen Feldern, die durch ein Skalen-Flugzeug-Modell induziert wurden


    Contributors:
    Grando, J. (author) / Labaune, G. (author) / Alliot, J.C. (author) / Issac, F. (author) / Delannoy, A. (author)

    Published in:

    Publication date :

    1989


    Size :

    4 Seiten


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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