Plasma Modeling for Aerospace Applications

ORAL · Invited

Abstract

The modeling of plasmas at atmospheric pressure is challenging due to the many physical phenomena involved and the transient and multiscale character of high-pressure discharges. Yet, it is a very promising tool for many industrial applications. In this presentation, plasma modeling for aerospace applications are focused on. First, plasma modeling can be used to explore promising technologies that are considered for future engine or aircraft designs. MHD (MagnetoHydroDynamics) and out-of-equilibrium plasma models will be described that make it possible to study into details many promising plasma actuator technologies for plasma assisted combustion and flow control in various Mach regimes. Second, plasma models are already employed in the aerospace industry as natural plasma discharges such as lightning may induce important constraints on aerospace structures. As an example, the modeling of lightning stroke to aircraft will be emphasized in the context of lightning safety. Finally, challenging issues in high pressure plasma modeling and numerical strategies that are currently under development will be discussed. The goal is to improve the versatility of current plasma models and to extend the range of applications that may benefit from predictive plasma and MHD numerical simulations.

Publication: Bourlet et al 2024 Plasma Sources Sci. Technol. 33 015010, "Numerical model of restrikes in gliding arc discharges", DOI 10.1088/1361-6595/ad1b6d.

Khiar et al 2023, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "Modelling of MHD flow control for atmospheric re-entry at ONERA", DOI: 10.13009/EUCASS2023-929.

Tholin et al 2023, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "Multiphase MHD model for electric explosions: Application to lightning protection systems", DOI: 10.13009/EUCASS2023-736.

Barreau et al 2023, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "Semi-implicit scheme for modelling the fluid dynamics part of a DC-powered arc.", DOI: 10.13009/EUCASS2023-684.

Tkachenko et al 2023, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "Resistive MHD simulations of a self-field magneto-plasmadynamic thruster over the 5 to 40 kA current range", DOI: 10.13009/EUCASS2023-562.

Pachoud et al 2023, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "Modelling of plasma discharge for aerospace applications: Streamer to arc transition", DOI:10.13009/EUCASS2023-882.

Pechereau et al, Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS, "3D modeling of an arc in interaction with a composite panel", DOI: 10.13009/EUCASS2023-701.

Sousa Martins et al 2016, J. Phys. D: Appl. Phys. 49 415205, "Characterization of a high current pulsed arc using optical emission spectroscopy", DOI 10.1088/0022-3727/49/41/415205.

Presenters

  • Fabien Tholin

    ONERA

Authors

  • Fabien Tholin

    ONERA