https://ieeexplore.ieee.org/abstract/document/10195992

*Authors*
Pol Fontanes, <https://orcid.org/0000-0001-8185-6350>Benjamin C.
Martell, Hector
Candela, Carmen Guerra-Garcia, Joan Montanya

*Citation*: P. Fontanes, B. C. Martell, H. Candela, C. Guerra-Garcia and J.
Montanya, "An experimental study of ion release from aircraft for
applications to electrostatic charge control and geoengineering," in *IEEE
Transactions on Aerospace and Electronic Systems*, doi:
10.1109/TAES.2023.3299438.

*27 July 2023*

Abstract:This paper presents an experimental study of an active
electrostatic charge control system for aircraft during the transient state
of ion release. We use an electrically isolated wing in a wind tunnel to
simulate an aircraft in flying conditions. We quantify the temporal
evolution of ion emission during the charging phase for different airspeeds
and applied potentials and provide spatially-resolved measurements of the
ion plume divergence. From the measurements, we explain the current
induction at the ion collector screen in response to the emitted ions. We
find that the duration of the transient state of ion emission depends on
the airspeed and is in the order of hundreds of milliseconds. For the
experimental conditions tested, we emit up to $±1μ$C , and reach ion
densities a few meters downstream of the source of order 1-10 nC/m 3 .
These values are sufficient to charge a body of 50 pF capacitance to
$±20$kV and reach space charge densities that could theoretically lead to
effective cloud charge modification. The study shows that ion plume
divergence and charge emission levels depend on the coronating electrode
configuration and geometry. For our setup, needle electrodes can emit
higher amounts of charge and lead to more concentrated ion beams, while
wire electrodes have a uniform spatial charge density emission. Finally, we
verify a numerical model against the experimental results to act as a
digital twin and use it to compute the optimal coronating electrode
position in terms of total emitted charge and charging levels acquired.

*Source: IEEE Xplore*

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